2007 October 5 - 22:02 GMT - Launch Site: Kourou. Launch Complex: ELA3. Launch Pad: -. Launch Vehicle: Ariane 5. Model: Ariane 5GS. LV Configuration: Ariane 5GS V178 (526). -
Optus D-2 Nation: Australia. Class: Communications. Spacecraft: Star bus. Manufacturer: Orbital. Agency: Optus. Perigee: 35,862 km (22,283 mi). Apogee: 35,889 km (22,300 mi). Inclination: 0.00 deg. Period: 1,440.70 min. COSPAR: 2007-044A. USAF Sat Cat: 32252. Ku-band satellite designed to deliver television, internet, communications, and data services to Australia and New Zealand. After deployment of the two satellites, the EPS third stage made a brief burn at 23:28 GMT to make the first in-flight test the Aestus engine's restart capability. This was to be used in 2008 in the first launch of the ATV ISS resupply spacecraft.
References: 2.
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Intelsat IS-11 Nation: USA. Program: Intelsat. Class: Communications. Spacecraft: Star bus. Manufacturer: Orbital. Agency: Intelsat. Perigee: 35,778 km (22,231 mi). Apogee: 35,797 km (22,243 mi). Inclination: 0.10 deg. Period: 1,436.10 min. COSPAR: 2007-044B. USAF Sat Cat: 32253. C and Ku-band satellite designed to provide Atlantic region communications services. References: 2.
2007 October 10 - 13:22 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz FG. LV Configuration: Soyuz-FG Ts15000-020. -
Soyuz TMA-11 Nation: Russia. Program: ISS. Payload: Soyuz TMA s/n 221 / ISS 15S. Mass: 7,200 kg (15,800 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz TMA. Perigee: 340 km (210 mi). Apogee: 344 km (213 mi). Inclination: 51.60 deg. Period: 91.40 min. COSPAR: 2007-045A. USAF Sat Cat: 32256. Duration: 191.80 days. Crew: Whitson, Malenchenko, Muszaphar. Flight: ISS EO-16, ISS EP-13. Soyuz TMA-11 delivered the EO-16 crew of Whitson and Malenchenko and EP-13 space tourist Shukor to the International Space Station. The Soyuz docked at the Zarya module at 14:50 GMT on 12 October. Whitson was EO-16 commander, with third astronaut Clay Anderson remaining aboard the station after the EO-15 crew and Shukor returned to earth on Soyuz TMA-10.Malenchenko and Whitson, together with visiting Korean astronaut Yi, who had been delivered to the ISS by Soyuz TMA-12, undocked from the station aboard Soyuz TMA-11 at 05:06 GMT on 19 April 2008. Following the deorbit burn at 07:40 GMT the aft service module of the Soyuz failed to separate and the spacecraft began re-entry in a reversed position, with the forward hatch taking the initial re-entry heating. As was the case with Soyuz 5 in 1970, the connections with the service module finally melted away, and the freed capsule righted itself aerodynamically with the heat shield taking the brunt of the re-entry heating. However the crew experienced a rough ride, a ballistic re-entry of over 8 G's force, smoke in the cabin, a failure of the soft landing system, and a very hard landing. They landed 470 km short of the target point at 50 deg 31" N, 61 deg 7" E at 08:29 GMT. A small grass fire was started at the landing point and the injured crew had to be helped from the capsule by passers-by. Malenchenko and Whitson suffered no permanent injury, but Yi was hit by Whitson's personal effects bag on impact and required physical therapy for neck and spine injuries.
References: 2.
2007 October 11 - 00:22 GMT - Launch Site: Cape Canaveral. Launch Complex: LC41. Launch Pad: SLC41. Launch Vehicle: Atlas V. Model: Atlas V 421. LV Configuration: Atlas V 421 AV-011. -
USA 195 Nation: USA. Payload: WGS SV-1. Class: Communications. Spacecraft: HS 702. Perigee: 32,586 km (20,247 mi). Apogee: 39,016 km (24,243 mi). Inclination: 0.20 deg. Period: 1,436.80 min. COSPAR: 2007-046A. USAF Sat Cat: 32258. First USAF Wideband Global Satcom satellite, designed to replace the DSCS series, was placed by the Atlas booster in an initial 477 km x 66,847 km x 20.1 deg geosynchronous transfer orbit. The satellite carried X-band and Ka-band communications payloads. References: 2.
2007 October 17 - 12:23 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: SLC17A. Launch Vehicle: Delta. Model: Delta 7925. LV Configuration: Delta 7925-9.5 D328. -
USA 196 Nation: USA. Program: Navstar. Payload: GPS 2R-17M / Navstar 55. Mass: 2,032 kg (4,479 lb). Class: Navigation. Spacecraft: GPS Block 2R. Manufacturer: Lockheed Martin Space Systems. Agency: U.S. Air Force. Perigee: 20,149 km (12,519 mi). Apogee: 20,213 km (12,559 mi). Inclination: 54.90 deg. Period: 717.90 min. COSPAR: 2007-047A. USAF Sat Cat: 32260. Set operational at 22:46 GMT on 31 October. References: 2.
2007 October 20 - 20:12 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz FG. LV Configuration: Soyuz-FG/Fregat Ts15000-022. -
Globalstar FM66 Nation: USA. Mass: 450 kg (990 lb). Class: Communications. Spacecraft: Globalstar. Manufacturer: SS/Loral. Agency: Globalstar. Perigee: 914 km (567 mi). Apogee: 932 km (579 mi). Inclination: 52.00 deg. Period: 103.50 min. COSPAR: 2007-048A. USAF Sat Cat: 32266. Last of the first generation Globalstar satellites, launched to replenish the constellation. The Fregat stage made three burns to deploy the satellites into circular orbit, and then deorbit itself to a reentry over the Pacific Ocean. References: 2.
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Globalstar FM67 Nation: USA. Mass: 450 kg (990 lb). Class: Communications. Spacecraft: Globalstar. Manufacturer: SS/Loral. Agency: Globalstar. Perigee: 925 km (574 mi). Apogee: 935 km (580 mi). Inclination: 52.00 deg. Period: 103.60 min. COSPAR: 2007-048B. USAF Sat Cat: 32265. References: 2.
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Globalstar FM68 Nation: USA. Mass: 450 kg (990 lb). Class: Communications. Spacecraft: Globalstar. Manufacturer: SS/Loral. Agency: Globalstar. Perigee: 915 km (568 mi). Apogee: 930 km (570 mi). Inclination: 52.00 deg. Period: 103.50 min. COSPAR: 2007-048C. USAF Sat Cat: 32264. References: 2.
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Globalstar FM70 Nation: USA. Mass: 450 kg (990 lb). Class: Communications. Spacecraft: Globalstar. Manufacturer: SS/Loral. Agency: Globalstar. Perigee: 911 km (566 mi). Apogee: 931 km (578 mi). Inclination: 52.00 deg. Period: 103.40 min. COSPAR: 2007-048D. USAF Sat Cat: 32263. References: 2.
2007 October 21 - 10:36 GMT -
2007 October 23 - 04:39 GMT - Launch Site: Plesetsk. Launch Complex: LC16/2. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M-2BL. -
Cosmos 2430 Nation: Russia. Mass: 1,900 kg (4,100 lb). Class: Early Warning. Spacecraft: Oko. Manufacturer: NPO Lavochkin. Agency: VKS. Perigee: 520 km (320 mi). Apogee: 39,175 km (24,342 mi). Inclination: 62.90 deg. Period: 704.50 min. COSPAR: 2007-049A. USAF Sat Cat: 32268. Missile early warning satellite References: 2.
2007 October 23 - 15:38 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39A. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-120. -
STS-120 Nation: USA. Program: ISS. Payload: Discovery F33 / Harmony / ISS-10A. Class: Manned. Type: Spaceplane. Spacecraft: Discovery. Agency: NASA. Perigee: 340 km (210 mi). Apogee: 344 km (213 mi). Inclination: 51.60 deg. Period: 91.40 min. COSPAR: 2007-050A. USAF Sat Cat: 32272. Duration: 15.10 days. Crew: Melroy, Zamka, Parazynski, Wheelock, Wilson, Nespoli, Tani. Flight: STS-120, ISS EO-15, ISS EO-16, ISS EO-16-1, ISS EO-15-1. Main mission objectives were delivery of the Harmony module to the station, and external work to move the P6 truss to its final location and put the ISS into its full-power configuration for the first time. Discovery docked with the ISS at the Destiny module at 12:40 GMT on 25 October. The cargo of 17,390 kg was as follows:
- Orbiter Docking System - Bay 1-2 - 1800 kg
- Spacesuit EMU 3004 - 130 kg
- Spacesuit EMU 3003 - 130 kg
- Station Power Distribution Unit SPDU - Bay 3P - 100 kg
- Fixture for return of S-band Antenna - SASA FSE - Bay 3P - 4S - 100 kg
- Power/Data Grapple Fixture for Node-2 - PDGF - Bay 5P - 50 kg
- Main Bus Switching Unit - MBSU - Bay 6S - 238 kg
- MBSU adapter - Bay 6S - 122 kg
- Station Power Distribution Unit - SPDU - Bay 6S - 7P - 100 kg
- Node-2 Harmony module - Bays 8-12 - 14,300 kg
- OBSS 203 - Sill 450 kg
- RMS 301 - Sill 410 kg
References: 2.
2007 October 24 - 10:05 GMT - Launch Site: Xichang. Launch Complex: LC1. Launch Pad: LC1?. Launch Vehicle: CZ. Model: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-15 (103). -
Chang'e-1 Nation: China. Class: Planetary. Type: Lunar. Spacecraft: Chang'e. Perigee: 147 km (91 mi). Apogee: 50,182 km (31,181 mi). Inclination: 30.80 deg. Period: 929.20 min. COSPAR: 2007-051B. USAF Sat Cat: 32273. China's first unmanned lunar/planetary probe. The initial orbit of 221 x 50,602 km x 31.0 deg was raised to a translunar trajectory by 31 October in a serious of spacecraft engine burns. The spacecraft entered a 210 km x 8600 km lunar orbit at 03:37 GMT on 5 November.
References: 2.
2007 October 26 - 07:35 GMT - Launch Site: Baikonur. Launch Complex: LC81/24. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 410-17. -
Cosmos 2431 Nation: Russia. Payload: Glonass-M s/n 718. Class: Navigation. Spacecraft: Glonass. Manufacturer: NPO-PM. Agency: KNITs. Perigee: 19,128 km (11,885 mi). Apogee: 19,130 km (11,880 mi). Inclination: 64.90 deg. Period: 675.70 min. COSPAR: 2007-052A. USAF Sat Cat: 32275. Three Uragan-M satellites were launched to replenish the Glonass navigation system, placed in GLONASS orbit plane 3. Cosmos 2431 set to operational on 4 December; plane/slot 3/17, frequency channel -1 References: 2.
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Cosmos 2432 Nation: Russia. Payload: Glonass-M s/n 719. Class: Navigation. Spacecraft: Glonass. Manufacturer: NPO-PM. Agency: KNITs. Perigee: 19,121 km (11,881 mi). Apogee: 19,135 km (11,889 mi). Inclination: 64.90 deg. Period: 675.70 min. COSPAR: 2007-052B. USAF Sat Cat: 32276. Set to operational; plane/slot 3/20, frequency channel 2 on 27 November. References: 2.
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Cosmos 2433 Nation: Russia. Payload: Glonass-M s/n 720. Class: Navigation. Spacecraft: Glonass. Manufacturer: NPO-PM. Agency: KNITs. Perigee: 19,121 km (11,881 mi). Apogee: 19,135 km (11,889 mi). Inclination: 64.90 deg. Period: 675.70 min. COSPAR: 2007-052C. USAF Sat Cat: 32277. Set to operational; plane/slot 3/19, frequency channel 3 on 25 November. References: 2.
2007 October 26 - 10:02 GMT - -
EVA STS-120-1 Nation: USA. Program: ISS. Crew: Parazynski, Wheelock. Flight: STS-120, ISS EO-16, ISS EO-16-1. EVA Duration: 0.25 days. The astronauts emerged from the Quest hatch at 10:01 GMT. They moved an antenna from the Z1 truss and stowed it in the payload bay, prepared the P6 truss for separation from Z1, and assisted in installation of the Harmony module, which was unberthed from the shuttle bay by the ISS Canadarm-2 and docked to the Unity module.
2007 October 28 - 09:32 GMT - -
EVA STS-120-2 Nation: USA. Program: ISS. Crew: Parazynski, Tani. Flight: STS-120, ISS EO-16, ISS EO-16-1. EVA Duration: 0.27 days. The astronauts emerged from the Quest hatch at 09:32 GMT. They assisted in unberthing of the P6 truss and its placement in a parked position. They also installed handrails and a grapple fixture on Harmony and inspected the malfunctioning Solar Array Rotary Joint (SARJ) on the S3/S4 truss.
2007 October 30 - 08:45 GMT - -
EVA STS-120-3 Nation: USA. Program: ISS. Crew: Parazynski, Wheelock. Flight: STS-120, ISS EO-16, ISS EO-16-1. EVA Duration: 0.29 days. The astronauts emerged from the Quest hatch at 08:44 GMT. They assisted in the mating of the P6 to P5 trusses and deployment of a radiator from P6. Wheelock transferred a spare Main Bus Switching Unit (MBSU) from the Shuttle bay to the External Stowage Platform 3 (ESP3). P6 solar array wing 2B was successfully redeployed; but deployment of array 4B had to be halted when a tear developed in the solar panel.
2007 November 1 - 00:51 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 11K65M-SL. -
SAR-Lupe 3 Nation: Germany. Mass: 770 kg (1,690 lb). Class: Surveillance. Type: Radarsat. Spacecraft: SAR-Lupe. Perigee: 474 km (294 mi). Apogee: 496 km (308 mi). Inclination: 98.20 deg. Period: 94.30 min. COSPAR: 2007-053A. USAF Sat Cat: 32283. Third SAR-Lupe radar satellite. The final stage also carried a small Automatic Identification System package by OHB/Bremen, designed to test a system for monitoring shipping traffic. Orbital plane ascending node 272 deg. References: 2.
2007 November 3 - 10:03 GMT - -
EVA STS-120-4 Nation: USA. Program: ISS. Crew: Parazynski, Wheelock. Flight: STS-120, ISS EO-16, ISS EO-16-1. EVA Duration: 0.30 days. The astronauts emerged from the Quest hatch and rode the ISS Canadarm II 50 m out to the snagged P6 solar array. Parazynski cut a snagged wire and installed homemade stabilizers designed to strengthen the array’s structure and stability in the vicinity of the damage. Wheelock helped from the truss by keeping an eye on the distance between Parazynski and the array. Afterwards they observed as ground controllers completed successful extension of the array.
2007 November 7 - 18:01 GMT -
2007 November 9 - 09:54 GMT - -
EVA ISS EO-16-1 Nation: USA. Program: ISS. Crew: Whitson, Malenchenko. Flight: ISS EO-16, ISS EO-16-1. EVA Duration: 0.29 days. The astronauts conducted exterior work in preparation for the move of the Pressurized Mating Adapter 2 (PMA-2) from the Destiny lab and to the Harmony module. They disconnected and stowed cables, removed a light on one of the station’s transport carts and took the cover off Harmony's Common Berthing Mechanism. They also removed a base-band signal processor for later refurbishment; removed a remote power controller module that was to be replaced; and transferred tools in preparation for upcoming spacewalks.
2007 November 11 - 01:50 GMT - Launch Site: Cape Canaveral. Launch Complex: LC37B. Launch Pad: SLC37B. Launch Vehicle: Delta IV. Model: Delta IV Heavy. LV Configuration: Delta 4H D4-8 (329) 4050H. -
USA 197 Nation: USA. Payload: DSP-1 Block 18 F23. Mass: 2,270 kg (5,000 lb). Class: Early Warning. Spacecraft: DSP. Manufacturer: Northrop Grumman Space Technology. Agency: National Security Agency. Perigee: 35,800 km (22,200 mi). Apogee: 36,325 km (22,571 mi). Inclination: 0.00 deg. Period: 1,436.00 min. COSPAR: 2007-054A. USAF Sat Cat: 32287. Final DSP launch. The series was to be replaced by SBIRS, which was in the middle of a troubled development program. The Delta 4H performed well after problems on its first launch. The RL10-powered upper stage made three burns before releasing the early-warning satellite in its final geosynchronous orbit. Total cost of the flight was $700 million, with the DSP worth $400 million. The DSP carried a special 25 kg supplementary payload designed to detect extremely small nuclear tests in space. The payload was required by a secret White House/National Security Council directive to detect any attempted covert nuclear tests by Iran or North Korea.
References: 2.
2007 November 11 - 22:48 GMT - Launch Site: Taiyuan. Launch Complex: -. Launch Pad: -. Launch Vehicle: CZ. Model: CZ-4C. LV Configuration: Chang Zheng 4C CZ4C (104). -
Yaogan 3 Nation: China. Mass: 2,700 kg (5,900 lb). Class: Radarsat. Type: Surveillance. Spacecraft: Yaogan. Perigee: 628 km (390 mi). Apogee: 629 km (390 mi). Inclination: 97.80 deg. Period: 97.30 min. COSPAR: 2007-055A. USAF Sat Cat: 32289. The military launch used a new version of the CZ-4 booster. The CZ-4C includes a restart capability in the upper stage and a new interstage adapter between the first and second stages. References: 2.
2007 November 14 - 22:06 GMT - Launch Site: Kourou. Launch Complex: ELA3. Launch Pad: -. Launch Vehicle: Ariane 5. Model: Ariane 5ECA. LV Configuration: Ariane 5ECA V179 (538). -
Star One C1 Nation: Brazil. Program: Brasilsat. Class: Communications. Spacecraft: Spacebus 3000. Agency: Embratel. Perigee: 35,794 km (22,241 mi). Apogee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 2007-056A. USAF Sat Cat: 32293. Formerly named Brasilsat C1, the satellite was launched as part of a joint venture between several South American countries with Brazil's Embratel taking a lead role. References: 2.
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Skynet 5B Nation: UK. Program: Skynet. Mass: 4,635 kg (10,218 lb). Class: Communications. Type: Military. Spacecraft: Eurostar 3000. Agency: Paradigm. Perigee: 35,784 km (22,235 mi). Apogee: 35,789 km (22,238 mi). Inclination: 0.10 deg. Period: 1,436.10 min. COSPAR: 2007-056B. USAF Sat Cat: 32294. Skynet 5B was designed to provide communications services in the SHF and UHF bands to the UK Ministry of Defence. References: 2.
2007 November 17 - 22:39 GMT - Launch Site: Baikonur. Launch Complex: LC200/39. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-M/Briz-M. -
Sirius 4 Nation: Sweden. Program: Sirius. Payload: A2100AX. Mass: 4,600 kg (10,100 lb). Class: Communications. Spacecraft: AS 2100. Manufacturer: Lockheed Martin, Sunnyvale. Perigee: 35,641 km (22,146 mi). Apogee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,432.20 min. COSPAR: 2007-057A. USAF Sat Cat: 32299. Sirius 4 carried Ku-band and Ka-band communications payloads for Nordic, Baltic and East European communications. Three upper-stage burns placed Sirius 4 into a 6916 km x 35478 km x 17.4 deg geostationary transfer orbit. A series of maneuvers by the satellite using its own Leros engine maneuvered the satellite into geosynchronous orbit, stationed at 5 deg East.
References: 2.
2007 December 9 - 00:15 GMT - Launch Site: Baikonur. Launch Complex: LC81/24. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-M/Briz-M. -
Cosmos 2434 Nation: Russia. Class: Communications. Type: Military. Spacecraft: Raduga-1. Perigee: 35,772 km (22,227 mi). Apogee: 35,802 km (22,246 mi). Inclination: 0.10 deg. Period: 1,436.10 min. COSPAR: 2007-058A. USAF Sat Cat: 32373. Raduga-1 / Globus communications satellite. References: 2.
2007 December 9 - 02:31 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 7420-10. LV Configuration: Delta 7420-10 D330. -
Cosmo-SkyMed 2 Nation: Italy. Mass: 1,700 kg (3,700 lb). Class: Surveillance. Type: Radarsat. Spacecraft: Cosmo-SkyMed. Manufacturer: Thales Alenia Space. Agency: ASI. Perigee: 621 km (385 mi). Apogee: 624 km (387 mi). Inclination: 97.90 deg. Period: 97.20 min. COSPAR: 2007-059A. USAF Sat Cat: 32376. Second Italian military radar satellite in the Cosmo-Skymed system. References: 2.
2007 December 10 - 22:05 GMT - Launch Site: Cape Canaveral. Launch Complex: LC41. Launch Pad: SLC41. Launch Vehicle: Atlas V. Model: Atlas V 401. LV Configuration: Atlas V 401 AV-015. -
USA 198 Nation: USA. Payload: NROL-24. Class: Communications. Type: Military. Spacecraft: SDS-3. Perigee: 515 km (320 mi). Apogee: 39,705 km (24,671 mi). Inclination: 62.60 deg. COSPAR: 2007-060A. USAF Sat Cat: 32378. Classified National Reconnaisance Office payload; probable primary payload data relay communications. May also have carried SBIRS HEO-2 infrared missile warning sensor and a TWINS-B magnetospheric research experiment. Initial orbit 261 x 16776 km x 60.0 deg.
References: 2.
2007 December 14 - 13:17 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz FG. LV Configuration: Soyuz-FG/Fregat Ts15000-025. -
Radarsat-2 Nation: Canada. Mass: 2,200 kg (4,800 lb). Class: Surveillance. Type: Radarsat. Spacecraft: Radarsat. Perigee: 791 km (491 mi). Apogee: 793 km (492 mi). Inclination: 98.60 deg. Period: 100.70 min. COSPAR: 2007-061A. USAF Sat Cat: 32382. Follow-on to Canadian Radarsat-1 launched in 1995. Designed to provide C-band synthetic aperture radar mapping with resolution of 3 m to Canadian government users. Compared to the earlier model had greater resolution, vastly increased on-board data storage capacity, and capability to scan left or right of ground track. Planned lifetime of seven years.
References: 2.
2007 December 18 - 09:50 GMT - -
EVA ISS EO-16-4 Nation: USA. Program: ISS. Crew: Whitson, Tani. Flight: ISS EO-16. EVA Duration: 0.29 days. The astronauts inspected the malfunctioning solar array rotation joint and beta gimbal assembly.
2007 December 20 - 20:04 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: SLC17A. Launch Vehicle: Delta. Model: Delta 7925. LV Configuration: Delta 7925-9.5 D331. -
USA 199 Nation: USA. Program: Navstar. Payload: GPS 2R-5M / Navstar 61. Class: Navigation. Spacecraft: GPS Block 2R. Manufacturer: Lockheed Martin Space Systems. Perigee: 20,082 km (12,478 mi). Apogee: 20,283 km (12,603 mi). Inclination: 55.00 deg. Period: 718.00 min. COSPAR: 2007-062A. USAF Sat Cat: 32384. Fifth GPS SV with L2C capability. References: 2.
2007 December 21 - 21:41 GMT - Launch Site: Kourou. Launch Complex: ELA3. Launch Pad: -. Launch Vehicle: Ariane 5. Model: Ariane 5GS. LV Configuration: Ariane 5GS V180 (530). - Rascom-QAF-1 Nation: Mauritius. Payload: Spacebus 4000B3. Mass: 4,579 kg (10,094 lb). Class: Communications. Spacecraft: Spacebus 4000. Manufacturer: Thales Alenia Space. Agency: RascomStarQAF. Perigee: 35,771 km (22,227 mi). Apogee: 35,796 km (22,242 mi). Inclination: 0.10 deg. Period: 1,436.00 min. COSPAR: 2007-063A. USAF Sat Cat: 32387. African communications satellite with a hybrid Ku/C-band payload. Nominal owner RascomStarQAF of Port Louis, Mauritius, a subsidiary of the Regional African Satellite Communications Organization (RASCOM) based in Cote d'Ivoire. The mission and satellite control centers were located in Cameroun and Libya. The satellite was to provide voice, data and internet services throughout Africa. Ahelium leak in the propulsion system prevented use of the primary apogee motor. Reaction control motors were used instead to slowly move the satellite into geosynchronous orbit. The satellite was expected to reach its operating location, but with a shorter-than-planned operational lifetime.
References: 2.
- Horizons 2 Nation: Bermuda. Payload: Star-2. Mass: 2,350 kg (5,180 lb). Class: Communications. Spacecraft: Star bus. Manufacturer: Orbital. Agency: Intelsat/Jsat. Perigee: 35,815 km (22,254 mi). Apogee: 35,816 km (22,254 mi). Inclination: 0.00 deg. Period: 1,437.50 min. COSPAR: 2007-063D. USAF Sat Cat: 32388. Launched by Horizons Satellite Holdings LLC, a joint venture of Intelsat and the Japanese JSAT company. To be placed at 74 deg W to serve United States, eastern Canada, and the Caribbean with communication services using its 16-transmitter Ku-band communications payload.
References: 2.
2007 December 23 - 07:12 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz-U. LV Configuration: ISS-27P. -
Progress M-62 Nation: Russia. Program: ISS. Payload: Progress M s/n 362. Class: Manned. Type: Logistics. Spacecraft: Progress M. Manufacturer: RKK Energia. Agency: Roskosmos. Perigee: 333 km (206 mi). Apogee: 341 km (211 mi). Inclination: 51.60 deg. Period: 91.30 min. COSPAR: 2007-064B. USAF Sat Cat: 32391. Duration: 54.11 days. Flight: ISS EO-16. Resupply spacecraft that docked with the Pirs port of the International Space Station at 08:14 GMT on 26 December. Undocked on 4 February 2008 at 10:32 GMT and then carried out Earth observations for ten days before being deorbited on 15 February at 09:44 GMT.
References: 2.
2007 December 25 - 19:32 GMT - Launch Site: Baikonur. Launch Complex: LC81/24. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-M/DM-2. -
Cosmos 2437 Nation: Russia. Payload: Uragan-M s/n 23. Class: Navigation. Spacecraft: Glonass. Perigee: 19,123 km (11,882 mi). Apogee: 19,137 km (11,891 mi). Inclination: 64.70 deg. Period: 675.70 min. COSPAR: 2007-065A. USAF Sat Cat: 32393. Three GLONASS-M satellites lofted in a single launch - inserted in GLONASS orbit plane 2. This was the second launch to populate this plane. References: 2.
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Cosmos 2435 Nation: Russia. Payload: Uragan-M s/n 21. Class: Navigation. Spacecraft: Glonass. Perigee: 19,081 km (11,856 mi). Apogee: 19,179 km (11,917 mi). Inclination: 64.70 deg. Period: 675.70 min. COSPAR: 2007-065B. USAF Sat Cat: 32394. References: 2.
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Cosmos 2436 Nation: Russia. Payload: Uragan-M s/n 22. Class: Navigation. Spacecraft: Glonass. Perigee: 19,100 km (11,800 mi). Apogee: 19,150 km (11,890 mi). Inclination: 64.70 deg. Period: 675.70 min. COSPAR: 2007-065C. USAF Sat Cat: 32395. References: 2.
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