MT-135
MT-135
Credit - via Jean-Jacques Serra
Sounding rocket. Year: 1964. Family: Other Suborbital Vehicles. Country: Japan.

Miniature weather observation rocket, single stage vehicle.

Manufacturer: Nissan. Launches: 592. First Launch Date: 1964-03-29. Last Launch Date: 2001-03-21. Launch data is: incomplete. Payload: 10 kg (22 lb). Apogee: 61 km (37 mi). Liftoff Thrust: 8.130 kN (1,828 lbf). Total Mass: 68 kg (149 lb). Core Diameter: 0.14 m (0.44 ft). Total Length: 3.30 m (10.80 ft).

Model: MT-135. Family: Other Suborbital Vehicles. Country: Japan.

Single stage vehicle consisting of 1 x MT-135P

Model: MT-135P. Family: Other Suborbital Vehicles. Country: Japan.

Single stage vehicle consisting of 1 x MT-135P

The MT-135P flew 1119 times over a thirty year life, gathering meteorological data in the upper atmosphere from July 15, 1970 to March 21, 2001. IHI Aerospace Co., Ltd. was responsible for design, development and manufacture of the MT-135P.

Launches: 1119.

MT-135 Chronology

1964 March 29 - 02:12 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 PT-135-1.

  • Propellant Test mission Nation: Japan. Agency: ISAS. Apogee: 51 km (31 mi). References: 1144.
1964 July 24 - 02:07 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-001.
  • Aeronomy mission Nation: Japan. Apogee: 49 km (30 mi). References: 1592.
1964 November 14 - 02:10 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-002.
  • Aeronomy mission Nation: Japan. Apogee: 55 km (34 mi). References: 1592.
1964 November 15 - 07:10 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-003.
  • Aeronomy mission Nation: Japan. Apogee: 55 km (34 mi). References: 1592.
1965 March 9 - 02:10 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-004.
  • Aeronomy mission Nation: Japan. Apogee: 53 km (32 mi). References: 1592.
1965 March 11 - 02:07 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-005.
  • Aeronomy mission Nation: Japan. Apogee: 60 km (37 mi). References: 1592.
1965 March 11 - 07:07 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-006.
  • Aeronomy mission Nation: Japan. Apogee: 60 km (37 mi). References: 1592.
1965 July 8 - 02:26 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-007.
  • Aeronomy mission Nation: Japan. Apogee: 50 km (31 mi). References: 1592.
1965 July 8 - 11:10 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-008.
  • Aeronomy mission Nation: Japan. Apogee: 50 km (31 mi). References: 1592.
1965 July 12 - 02:07 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-009.
  • Aeronomy mission Nation: Japan. Apogee: 50 km (31 mi). References: 1592.
1965 September 29 - 02:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-010.
  • Aeronomy mission Nation: Japan. Apogee: 48 km (29 mi). References: 1592.
1965 September 29 - 07:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-011.
  • Aeronomy mission Nation: Japan. Apogee: 51 km (31 mi). References: 1592.
1966 January 18 - 02:10 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-012.
  • Aeronomy mission Nation: Japan. Apogee: 54 km (33 mi). References: 1592.
1966 January 19 - 10:30 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-014.
  • Aeronomy mission Nation: Japan. Apogee: 49 km (30 mi). References: 1592.
1966 January 19 - 02:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-013.
  • Aeronomy mission Nation: Japan. Apogee: 59 km (36 mi). References: 1592.
1966 April 30 - 02:20 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-015.
  • Aeronomy mission Nation: Japan. Apogee: 53 km (32 mi). References: 1592.
1966 April 30 - 10:40 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-016.
  • Aeronomy mission Nation: Japan. Apogee: 54 km (33 mi). References: 1592.
1966 May 2 - 02:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-017.
  • Aeronomy mission Nation: Japan. Apogee: 55 km (34 mi). References: 1592.
1966 August 11 - 05:30 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 IT-135-1.
  • Test mission Nation: Japan. Apogee: 45 km (27 mi). References: 1145.
1966 August 18 - 02:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-018.
  • Aeronomy mission Nation: Japan. Apogee: 52 km (32 mi). References: 1592.
1966 September 21 - 02:10 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 DT-135-1.
  • Test mission Nation: Japan. Apogee: 56 km (34 mi). References: 1145.
1966 October 13 - 02:25 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-019.
  • Aeronomy mission Nation: Japan. Apogee: 44 km (27 mi). References: 1592.
1966 October 13 - 04:20 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-A -020.
  • Aeronomy mission Nation: Japan. Apogee: 65 km (40 mi). References: 1592.
1967 January 19 - 02:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-021.
  • Aeronomy mission Nation: Japan. Apogee: 60 km (37 mi). References: 1592.
1967 January 22 - 05:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-023.
  • Aeronomy mission Nation: Japan. Apogee: 62 km (38 mi). References: 1592.
1967 January 22 - 02:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-022.
  • Aeronomy mission Nation: Japan. Apogee: 63 km (39 mi). References: 1592.
1967 January 22 - 08:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-024.
  • Aeronomy mission Nation: Japan. Apogee: 59 km (36 mi). References: 1592.
1967 January 24 - 02:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-025.
  • Aeronomy mission Nation: Japan. Apogee: 59 km (36 mi). References: 1592.
1967 March 31 - 18:28 GMT - Launch Site: Wallops Island. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135.
  • Aeronomy mission Nation: Japan. Agency: JMA?. Apogee: 54 km (33 mi). References: 1145.
1967 April 4 - 09:55 GMT - Launch Site: Wallops Island. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135.
  • Aeronomy mission Nation: Japan. Agency: NASA/JMA. Apogee: 57 km (35 mi). References: 1145.
1967 April 4 - 09:10 GMT - Launch Site: Wallops Island. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135.
  • Aeronomy mission Nation: Japan. Agency: NASA/JMA. Apogee: 54 km (33 mi). References: 1145.
1967 April 4 - 11:07 GMT - Launch Site: Wallops Island. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135.
  • Aeronomy mission Nation: Japan. Agency: NASA/JMA. Apogee: 54 km (33 mi). References: 1145.
1967 April 4 - 22:44 GMT - Launch Site: Wallops Island. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135.
  • Aeronomy mission Nation: Japan. Agency: NASA/JMA. Apogee: 56 km (34 mi). References: 1145.
1967 April 4 - 16:28 GMT - Launch Site: Wallops Island. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135.
  • Aeronomy mission Nation: Japan. Agency: NASA/JMA. Apogee: 55 km (34 mi). References: 1145.
1967 April 4 - 11:56 GMT - Launch Site: Wallops Island. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135.
  • Aeronomy mission Nation: Japan. Agency: NASA/JMA. Apogee: 57 km (35 mi). References: 1145.
1967 April 5 - 03:33 GMT - Launch Site: Wallops Island. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135.
  • Aeronomy mission Nation: Japan. Agency: NASA/JMA. Apogee: 56 km (34 mi). References: 1145.
1967 April 5 - 00:15 GMT - Launch Site: Wallops Island. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135.
  • Aeronomy mission Nation: Japan. Agency: NASA/JMA. Apogee: 56 km (34 mi). References: 1145.
1967 April 5 - 01:01 GMT - Launch Site: Wallops Island. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135.
  • Aeronomy mission Nation: Japan. Agency: NASA/JMA. Apogee: 54 km (33 mi). References: 1145.
1968 September 15 - 02:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-036.
  • Aeronomy mission Nation: Japan. Apogee: 55 km (34 mi). References: 1592.
1968 September 15 - 05:18 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-037.
  • Aeronomy mission Nation: Japan. Apogee: 56 km (34 mi). References: 1592.
1969 January 4 - 05:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-039.
  • Aeronomy mission Nation: Japan. Apogee: 59 km (36 mi). References: 1592.
1969 January 4 - 02:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-038.
  • Aeronomy mission Nation: Japan. Apogee: 57 km (35 mi). References: 1592.
1969 January 5 - 02:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-40.
  • Aeronomy mission Nation: Japan. Agency: ISAS. Apogee: 59 km (36 mi). References: 1592.
1969 January 5 - 05:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT-135P-1.
  • Aeronomy mission Nation: Japan. Agency: ISAS. Apogee: 44 km (27 mi). References: 1592.
1969 September 6 - 02:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-041.
  • Aeronomy mission Nation: Japan. Apogee: 59 km (36 mi). References: 1592.
1969 September 7 - 05:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-042.
  • Aeronomy mission Nation: Japan. Apogee: 57 km (35 mi). References: 1592.
1969 September 7 - 02:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT-135-P -002.
  • Aeronomy mission Nation: Japan. Apogee: 53 km (32 mi). References: 1592.
1969 September 27 - 02:05 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT-135-P -003.
  • Aeronomy mission Nation: Japan. Apogee: 52 km (32 mi). References: 1592.
1969 September 27 - 05:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. LV Configuration: MT-135 MT-135-043.
  • Aeronomy mission Nation: Japan. Apogee: 49 km (30 mi). References: 1592.
1970 January 22 - 05:00 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT-135-P -004.
  • Aeronomy mission Nation: Japan. Apogee: 53 km (32 mi). References: 1592.
1970 January 23 - 02:20 GMT - Launch Site: Kagoshima. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT-135-P -005.
  • Aeronomy mission Nation: Japan. Apogee: 53 km (32 mi). References: 1592.
1970 August 5 - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Range Test / Aeronomy mission Nation: Japan. Agency: JMA. Apogee: 60 km (37 mi). References: 1139.
1972 February 2 - 06:56 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T1.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1972 February 7 - 06:45 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T2.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1972 August 30 - 06:15 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T4.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1972 August 30 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T3.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1973 February 5 - 01:52 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T5.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1973 February 8 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T6.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1973 September 5 - 01:57 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T7.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1973 September 5 - 06:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T8.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1974 February 2 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T9.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1974 February 10 - 06:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T10.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1974 September 3 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T11.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1974 September 3 - 06:00 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T12.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1975 January 30 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T13.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1975 February 7 - 01:00 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T14.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1975 September 10 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T15.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1976 September 23 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T16.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1976 September 25 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T17.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1977 February 24 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T18.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1977 August 23 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T19.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1977 August 26 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T20.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1978 February 17 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T21.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1978 August 24 - 01:45 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T22.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1978 August 26 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T23.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1979 February 7 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T24.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1979 July 4 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1979 July 18 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1979 August 1 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1979 August 15 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1979 August 27 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T25.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1979 August 27 - 06:00 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T26.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1979 September 12 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1979 September 26 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1979 October 3 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 59 km (36 mi). References: 1580.
1979 October 17 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1979 October 24 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1979 November 7 - 02:14 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 59 km (36 mi). References: 1580.
1979 November 14 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1979 December 5 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1979 December 12 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1979 December 19 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1979 December 26 - 02:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1980 January 9 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1980 January 16 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1980 January 23 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1980 February 13 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1980 February 20 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1980 February 23 - 01:55 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T27.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1980 March 5 - 02:02 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1980 March 19 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1980 March 26 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1980 April 9 - 02:04 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1980 April 16 - 02:10 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1980 April 30 - 02:15 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1980 May 8 - 02:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1980 May 14 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1980 May 21 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1980 May 28 - 02:10 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1980 June 4 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1980 June 11 - 02:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1980 June 25 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 59 km (36 mi). References: 1580.
1980 July 23 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1980 August 6 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1980 August 20 - 02:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 59 km (36 mi). References: 1580.
1980 September 3 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1980 September 13 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T28.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1980 September 15 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T29.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1980 September 17 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1980 October 1 - 02:13 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1980 October 8 - 02:04 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1980 October 22 - 02:10 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1980 October 29 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 50 km (31 mi). References: 1580.
1980 November 12 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1980 November 26 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1980 December 3 - 02:02 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 59 km (36 mi). References: 1580.
1980 December 10 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 52 km (32 mi). References: 1580.
1980 December 17 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1980 December 19 - 11:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P R370.
  • Aeronomy mission? Nation: Japan. Agency: MT. Apogee: 64 km (39 mi). References: 1559.
1980 December 26 - 11:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P R371.
  • Aeronomy mission? Nation: Japan. Agency: MT. Apogee: 64 km (39 mi). References: 1559.
1981 January 7 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1981 January 14 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1981 January 22 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1981 January 28 - 02:29 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1981 February 4 - 02:04 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 59 km (36 mi). References: 1580.
1981 February 12 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T30.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1981 February 18 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1981 February 26 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 61 km (37 mi). References: 1580.
1981 March 11 - 02:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1981 March 18 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1981 March 26 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 52 km (32 mi). References: 1580.
1981 April 8 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1981 April 15 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1981 April 22 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1981 April 29 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1981 May 13 - 02:15 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1981 May 20 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1981 May 27 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1981 June 10 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1981 June 24 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1981 July 8 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1981 July 23 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1981 August 6 - 02:07 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1981 August 20 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1981 September 2 - 02:20 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1981 September 30 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1981 October 7 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 51 km (31 mi). References: 1580.
1981 October 28 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1981 November 11 - 02:02 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 52 km (32 mi). References: 1580.
1981 November 19 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1981 November 25 - 02:04 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1981 December 3 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1981 December 9 - 02:04 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1981 December 16 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1981 December 23 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1982 January 6 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1982 January 13 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1982 January 21 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 52 km (32 mi). References: 1580.
1982 January 27 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1982 February 2 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T31.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1982 February 3 - 02:15 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1982 February 3 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T32.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1982 February 17 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1982 February 24 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 45 km (27 mi). References: 1580.
1982 March 10 - 02:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 24 km (14 mi). References: 1580.
1982 March 17 - 02:20 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 49 km (30 mi). References: 1580.
1982 March 24 - 02:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1982 April 7 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1982 April 14 - 02:02 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1982 April 21 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1982 May 12 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1982 May 19 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 43 km (26 mi). References: 1580.
1982 May 26 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1982 June 2 - 02:02 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1982 June 9 - 02:02 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1982 June 23 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1982 July 7 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1982 July 21 - 02:25 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1982 August 5 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1982 August 18 - 02:12 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1982 September 1 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1982 September 5 - 01:30 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Vehicle: MT-135. Model: MT-135P. LV Configuration: MT-135P MT135P T33.
  • Aeronomy mission? Nation: Japan. Agency: NASDA. Apogee: 50 km (31 mi). References: 1904.
1982 September 8 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1982 September 15 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1982 September 29 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1982 October 7 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1982 October 21 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1982 October 27 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1982 November 10 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1982 November 18 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1982 December 2 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1982 December 8 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1982 December 15 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1982 December 29 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1983 January 12 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1983 January 19 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1983 January 26 - 02:18 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1983 February 3 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1983 February 16 - 02:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1983 February 23 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1983 March 9 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1983 March 16 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1983 March 23 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1983 April 6 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1983 April 13 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1983 April 20 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 59 km (36 mi). References: 1580.
1983 April 27 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1983 May 11 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1983 May 18 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1983 May 26 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1983 June 1 - 02:15 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1983 June 15 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 59 km (36 mi). References: 1580.
1983 June 29 - 02:04 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1983 July 14 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1983 July 27 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 59 km (36 mi). References: 1580.
1983 August 10 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1983 August 25 - 02:30 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1983 September 7 - 02:15 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1983 September 14 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 50 km (31 mi). References: 1580.
1983 October 12 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 51 km (31 mi). References: 1580.
1983 October 19 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 52 km (32 mi). References: 1580.
1983 October 26 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1983 November 2 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1983 November 16 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1983 November 30 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1983 December 7 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1983 December 14 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1983 December 21 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1983 December 28 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1984 January 11 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1984 January 19 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1984 January 25 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1984 February 8 - 02:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1984 February 15 - 02:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1984 February 22 - 02:02 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1984 March 7 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1984 March 14 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1984 March 28 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1984 April 11 - 02:02 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1984 April 18 - 02:10 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 49 km (30 mi). References: 1580.
1984 April 25 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1984 May 9 - 02:02 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1984 May 16 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 52 km (32 mi). References: 1580.
1984 May 23 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 51 km (31 mi). References: 1580.
1984 May 30 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 51 km (31 mi). References: 1580.
1984 June 13 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1984 June 20 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1984 July 4 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1984 July 18 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1984 August 1 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 52 km (32 mi). References: 1580.
1984 August 29 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1984 September 6 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1984 September 19 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1984 October 10 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1984 October 18 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1984 October 24 - 02:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1984 October 31 - 02:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1984 November 7 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1984 November 14 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1984 November 21 - 02:04 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 52 km (32 mi). References: 1580.
1984 December 5 - 02:04 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1984 December 12 - 02:20 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1984 December 19 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1985 January 9 - 02:04 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 53 km (32 mi). References: 1580.
1985 January 16 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1985 January 23 - 02:02 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1985 February 6 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1985 February 13 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1985 February 21 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1985 February 27 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1985 March 14 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1985 March 27 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1985 April 17 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1985 April 24 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1985 May 8 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1985 May 15 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1985 May 22 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 59 km (36 mi). References: 1580.
1985 May 30 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 59 km (36 mi). References: 1580.
1985 June 12 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 55 km (34 mi). References: 1580.
1985 June 20 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 56 km (34 mi). References: 1580.
1985 July 3 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1985 July 17 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 61 km (37 mi). References: 1580.
1985 July 31 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1985 September 11 - 02:01 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi). References: 1580.
1985 September 19 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 59 km (36 mi). References: 1580.
1985 October 2 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 51 km (31 mi). References: 1580.
1985 October 16 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1985 October 31 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi). References: 1580.
1985 November 6 - 02:03 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 46 km (28 mi). References: 1580.
1985 November 13 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.
  • Meteorological mission Nation: Japan. Agency: JMA. Apogee: 58 km (36 mi). References: 1580.
1985 November 20 - 02:00 GMT - Launch Site: Ryori. Launch Vehicle: MT-135. Model: MT-135P.