Chang Zheng 4C

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

Chang Zheng 4C

Part of CZ

Chinese orbital launch vehicle. The CZ-4C, first flown in 2007, had an upgraded second-stage engine that could be restarted in space. The vehicle also had structural rings at the base of the first and second stages, an interstage weather cover, ejected at liftoff, and the larger payload shroud introduced on the CZ-4B. All of these indicated that the vehicle was designed to take larger payloads to higher, more precise orbits than the CZ-4B.

AKA: Chang Zheng-4C;CZ-4C;Long March 4C. Status: Active. First Launch: 2006-04-26. Last Launch: 2018-05-20. Number: 25 . Payload: 2,800 kg (6,100 lb). Thrust: 2,960.00 kN (665,430 lbf). Gross mass: 250,000 kg (550,000 lb). Height: 45.80 m (150.20 ft). Diameter: 3.35 m (10.99 ft).

LEO Payload: 2,800 kg (6,100 lb). Payload: 2,800 kg (6,100 lb) to a 900 km SSO. Launch Price $: 35.000 million in 1999 dollars.

More at: Chang Zheng 4C.

Family: orbital launch vehicle. Country: China. Spacecraft: CAST3000, Oscar, SJ-6, FY-3, Ban Xing, JB-5, JB-9, JB-8. Launch Sites: Taiyuan LC9, Taiyuan, Jiuquan SLS-2, Taiyuan LC1. Agency: CALT.

2006 April 26 - . 22:48 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC1. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 1 - . Payload: Jianbing 5. Mass: 2,700 kg (5,900 lb). Nation: China. Agency: CNSA. Manufacturer: CASC. Class: Surveillance. Type: Military Radarsat. Spacecraft Bus: Jianbing. Spacecraft: JB-5. USAF Sat Cat: 29092 . COSPAR: 2006-015A. Apogee: 630 km (390 mi). Perigee: 627 km (389 mi). Inclination: 97.80 deg. Period: 97.30 min. Remote sensing satellite built by the Shanghai SAST Group. In reality it was the first Chinese synthetic aperture radar military surveillance satellite..

2007 November 11 - . 22:48 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 3 - . Payload: Jianbing 5. Mass: 2,700 kg (5,900 lb). Nation: China. Agency: SISE. Class: Surveillance. Type: Civilian Radarsat. Spacecraft Bus: Jianbing. Spacecraft: JB-5. USAF Sat Cat: 32289 . COSPAR: 2007-055A. Apogee: 629 km (390 mi). Perigee: 628 km (390 mi). Inclination: 97.80 deg. Period: 97.30 min. 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..

2008 May 27 - . 03:02 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

FY-3A - . Mass: 1,500 kg (3,300 lb). Nation: China. Agency: SISE. Class: Earth. Type: Weather satellite. Spacecraft: FY-3. USAF Sat Cat: 32958 . COSPAR: 2008-026A. Apogee: 828 km (514 mi). Perigee: 826 km (513 mi). Inclination: 98.80 deg. Period: 101.40 min. Polar orbiting weather satellite. The FY-3 series will replace the older FY-1 polar system..

2009 December 15 - . 02:31 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 8 - . Payload: Jianbing 9. Mass: 2,500 kg (5,500 lb). Nation: China. Agency: SISE. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Jianbing. Spacecraft: JB-9. USAF Sat Cat: 36121 . COSPAR: 2009-072A. Apogee: 1,204 km (748 mi). Perigee: 1,193 km (741 mi). Inclination: 100.50 deg. Period: 109.40 min. Sun-synchronous orbit low resolution imaging satellite, primarily for civilian Earth resource studies. Supplemental military missions may include weather forecasting..

Xi Wang 1 - . Mass: 50 kg (110 lb). Nation: China. Agency: SISE. Class: Communications. Type: Amateur radio communications satellite. Spacecraft: Oscar. USAF Sat Cat: 36122 . COSPAR: 2009-072B. Apogee: 1,205 km (748 mi). Perigee: 1,193 km (741 mi). Inclination: 100.50 deg. Period: 109.40 min. Amateur radio satellite..

2010 March 5 - . 04:55 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 9A - . Mass: 200 kg (440 lb). Nation: China. Agency: SISE. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 36413 . COSPAR: 2010-009A. Apogee: 1,107 km (687 mi). Perigee: 1,075 km (667 mi). Inclination: 63.40 deg. Period: 107.10 min.

Yaogan 9B - . Mass: 2,000 kg (4,400 lb). Nation: China. Agency: SISE. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 36414 . COSPAR: 2010-009B. Apogee: 1,107 km (687 mi). Perigee: 1,075 km (667 mi). Inclination: 63.40 deg. Period: 107.10 min.

Yaogan 9C - . Mass: 200 kg (440 lb). Nation: China. Agency: SISE. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 36415 . COSPAR: 2010-009C. Apogee: 1,107 km (687 mi). Perigee: 1,074 km (667 mi). Inclination: 63.40 deg. Period: 107.10 min.

2010 August 9 - . 22:49 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 10 - . Payload: Yaogan Weixing 10 / Jianbing 5. Mass: 2,700 kg (5,900 lb). Nation: China. Agency: SISE. Class: Surveillance. Type: Civilian Radarsat. Spacecraft Bus: Jianbing. Spacecraft: JB-5. USAF Sat Cat: 36834 . COSPAR: 2010-038A. Apogee: 630 km (390 mi). Perigee: 627 km (389 mi). Inclination: 97.80 deg. Period: 97.30 min. Radar imaging satellite..

2010 November 5 - . 18:37 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

FY-3B - . Payload: Fengyun 3 (01 B. Mass: 1,500 kg (3,300 lb). Nation: China. Class: Earth. Type: Weather satellite. Spacecraft: FY-3. USAF Sat Cat: 37214 . COSPAR: 2010-059A. Apogee: 828 km (514 mi). Perigee: 825 km (512 mi). Inclination: 98.70 deg. Period: 101.40 min. Second polar orbiting FY-3 weather satellite..

2012 May 29 - . 07:31 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 15 - . Payload: Jianbing 9. Mass: 2,500 kg (5,500 lb). Nation: China. Class: Surveillance. Type: Military Radarsat. Spacecraft Bus: Jianbing. Spacecraft: JB-9. USAF Sat Cat: 38354 . COSPAR: 2012-029A. Apogee: 1,207 km (749 mi). Perigee: 1,201 km (746 mi). Inclination: 100.10 deg. Period: 109.50 min.

2012 November 25 - . 04:06 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 16A - . Mass: 2,000 kg (4,400 lb). Nation: China. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 39011 . COSPAR: 2012-066A. Apogee: 1,096 km (681 mi). Perigee: 1,085 km (674 mi). Inclination: 63.40 deg. Period: 107.10 min. Believed to be a military naval SIGINT surveillance system, consisting of a main satellite and two subsatellites. Second such launch after 2010's Yaogan 9..

Yaogan 16B - . Mass: 200 kg (440 lb). Nation: China. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 39012 . COSPAR: 2012-066B. Apogee: 1,095 km (680 mi). Perigee: 1,086 km (674 mi). Inclination: 63.40 deg. Period: 107.10 min.

Yaogan 16C - . Mass: 200 kg (440 lb). Nation: China. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 39013 . COSPAR: 2012-066C. Apogee: 1,096 km (681 mi). Perigee: 1,085 km (674 mi). Inclination: 63.40 deg. Period: 107.10 min.

2013 July 19 - . 23:37 GMT - . Launch Site: Taiyuan. Launch Pad: xxx. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Shiyan 7 - . Mass: 800 kg (1,760 lb). Nation: China. Class: Surveillance. Type: Surveillance satellite. Spacecraft: CAST3000. USAF Sat Cat: 39208 . COSPAR: 2013-037A. Apogee: 674 km (418 mi). Perigee: 660 km (410 mi). Inclination: 98.04 deg. Period: 98.09 min. Satellite inspector with robotic arm. After maneuvering close to Chuangxin-3 on 6 and 9 August, it completed an unexpected rendezvous in a 564 x 610 km x 97.7 deg orbit with the Shi Jian 7 (SJ-7), launched in 2005..

Chuangxin 3 - . Mass: 40 kg (88 lb). Nation: China. Class: Technology. Type: Technology satellite. Spacecraft: Ban Xing. USAF Sat Cat: 39209 . COSPAR: 2013-037B. Apogee: 673 km (418 mi). Perigee: 665 km (413 mi). Inclination: 98.04 deg. Period: 98.12 min. Served as target for the Shiyan 7 satellite inspector / robotic arm test vehicle..

SJ-15 - . Mass: 2,700 kg (5,900 lb). Nation: China. Class: Technology. Type: Technology satellite. Spacecraft: SJ-6. USAF Sat Cat: 39210 . COSPAR: 2013-037C. Apogee: 608 km (377 mi). Perigee: 563 km (349 mi). Inclination: 97.68 deg. Period: 96.39 min.
Thought to be carrying out observations of space debris. Made a slight orbit adjustment of 1 km on 15 October to a 660 km x 675 km orbit, then released a new object, 2013-037J, with which it maintained stationkeeping within 2 km. The new object was perhaps a target subsatellite, possibly passive, for experiments with proximity operations.

2013 September 1 - . 19:16 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 17A - . Mass: 2,000 kg (4,400 lb). Nation: China. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 39239 . COSPAR: 2013-046A. Apogee: 1,116 km (693 mi). Perigee: 1,065 km (661 mi). Inclination: 63.41 deg. Period: 107.05 min.
Triplet of naval surveillance satellites, believed to operate like the old US PARCAE/NOSS system, in which a group of loosely formation-flying spacecraft locate radio emitters using the difference in time of arrival of the radio signals at the different satellites.

Yaogan 17B - . Mass: 200 kg (440 lb). Nation: China. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 39240 . COSPAR: 2013-046B. Apogee: 1,116 km (693 mi). Perigee: 1,065 km (661 mi). Inclination: 63.41 deg. Period: 107.05 min.

Yaogan 17C - . Mass: 200 kg (440 lb). Nation: China. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 39241 . COSPAR: 2013-046C. Apogee: 1,116 km (693 mi). Perigee: 1,064 km (661 mi). Inclination: 63.41 deg. Period: 107.05 min.

2013 September 23 - . 03:07 GMT - . Launch Site: Taiyuan. Launch Pad: LC9. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

FY-3-03 - . Payload: Fengyun-3C. Mass: 1,500 kg (3,300 lb). Nation: China. Class: Earth. Type: Weather satellite. Spacecraft: FY-3. USAF Sat Cat: 39260 . COSPAR: 2013-052A. Apogee: 828 km (514 mi). Perigee: 827 km (513 mi). Inclination: 98.77 deg. Period: 101.45 min. Third Fengyun-3 polar orbiting meteorological satellite..

2013 November 20 - . 03:31 GMT - . Launch Site: Taiyuan. Launch Pad: xxx. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 19 - . Payload: Jianbing 9. Mass: 2,500 kg (5,500 lb). Nation: China. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Jianbing. Spacecraft: JB-9. USAF Sat Cat: 39410 . COSPAR: 2013-065A. Apogee: 1,208 km (750 mi). Perigee: 1,201 km (746 mi). Inclination: 100.45 deg. Period: 109.51 min. Thought to be an imaging satellite similar to Yaogan 8..

2014 August 9 - . 05:45 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 20b - . Mass: 200 kg (440 lb). Nation: China. Agency: CASC. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 40110 . COSPAR: 2014-047B. Apogee: 1,094 km (679 mi). Perigee: 1,087 km (675 mi). Inclination: 63.40 deg. Period: 107.05 min.

Yaogan 20c - . Mass: 200 kg (440 lb). Nation: China. Agency: CASC. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 40111 . COSPAR: 2014-047C. Apogee: 1,094 km (679 mi). Perigee: 1,087 km (675 mi). Inclination: 63.40 deg. Period: 107.05 min.

Yaogan 20a - . Mass: 2,000 kg (4,400 lb). Nation: China. Agency: CASC. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 40109 . COSPAR: 2014-047A. Apogee: 1,066 km (662 mi). Perigee: 1,054 km (654 mi). Inclination: 63.40 deg. Period: 106.41 min. Triplet satellites, the fourth in a series; previous triplet clusters were Yaogan 9, 16 and 17. They were thought to be analogous to the old US NOSS/PARCAE ocean surveillance system..

2014 October 20 - . 06:31 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 22 - . Payload: Jianbing 9. Mass: 2,500 kg (5,500 lb). Nation: China. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Jianbing. Spacecraft: JB-9. USAF Sat Cat: 40275 . COSPAR: 2014-063A. Apogee: 1,207 km (749 mi). Perigee: 1,198 km (744 mi). Inclination: 100.36 deg. Period: 109.48 min. Sun synchronous orbit; 1330 GMT local time of the descending node..

2014 December 10 - . 19:33 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 25a - . Mass: 2,000 kg (4,400 lb). Nation: China. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 40338 . COSPAR: 2014-080A. Apogee: 1,106 km (687 mi). Perigee: 1,074 km (667 mi). Inclination: 63.41 deg. Period: 107.05 min. Fifth Yaogan mission. Each consisted of a main satellite and two subsatellites..

Yaogan 25b - . Mass: 200 kg (440 lb). Nation: China. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 40339 . COSPAR: 2014-080B. Apogee: 1,106 km (687 mi). Perigee: 1,074 km (667 mi). Inclination: 63.41 deg. Period: 107.05 min.

Yaogan 25c - . Mass: 200 kg (440 lb). Nation: China. Class: Surveillance. Type: Naval SIGINT. Spacecraft Bus: Jianbing. Spacecraft: JB-8. USAF Sat Cat: 40340 . COSPAR: 2014-080C. Apogee: 1,106 km (687 mi). Perigee: 1,074 km (667 mi). Inclination: 63.41 deg. Period: 107.05 min.

2015 August 27 - . 02:31 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC9. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 27 - . Payload: Jianbing 9. Mass: 2,500 kg (5,500 lb). Nation: China. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Jianbing. Spacecraft: JB-9. USAF Sat Cat: 40878 . COSPAR: 2015-040A. Apogee: 1,207 km (749 mi). Perigee: 1,193 km (741 mi). Inclination: 100.48 deg. Period: 109.43 min. The 27th Yaogan remote sensing satellite. Fifth in the Yaogan High A series and appeared to replace the first, Yaogan 8, in a sun synchronous orbit with a 09:30 local time longitude of descending node..

2015 November 26 - . 21:24 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 29 - . Nation: China. Class: Surveillance. Type: Military Radarsat. Spacecraft Bus: Jianbing. Spacecraft: JB-5. USAF Sat Cat: 41038 . COSPAR: 2015-069A. Apogee: 619 km (384 mi). Perigee: 615 km (382 mi). Inclination: 97.80 deg.
A new Yaogan satellite. The orbit was very similar to that of the Yaogan 1, 3 and 10 satellites though to be radar imaging vehicles developed by the Shanghai Academy of Space Technology (SAST). Placed in sun synchronous orbit with 04:30 Equator crossing time.

2016 August 9 - . 22:55 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Gaofen 3 - . Nation: China. Class: Surveillance. Type: Military Radarsat. USAF Sat Cat: 41727 . COSPAR: 2016-049A. Apogee: 751 km (466 mi). Perigee: 750 km (460 mi). Inclination: 98.40 deg. A 1-meter-resolution C-band radar imaging satellite placed in 750 km 0600LT sun-synchronous orbit. Its primary user was the National Satellite Oceanic Applications Center in Mudanjiang..

2016 August 31 - . 18:55 GMT - . Launch Site: Taiyuan. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

GaoFen 10 - . Nation: China. Class: Surveillance. Type: Surveillance satellite. COSPAR: 2016-0F01. High resolution imaging satellite lost in the launch failure. Rumored third stage restart failure, which would have left the vehicle just short of a marginal orbit..

2017 November 14 - . 18:34 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC9. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Feng Yun 3D - . Payload: di si ke fengyun sanhao. Nation: China. USAF Sat Cat: 43010 . COSPAR: 2017-072A. Apogee: 828 km (514 mi). Perigee: 824 km (512 mi). Inclination: 98.70 deg. Period: 101.43 min. See FY 3D. ..

HEAD-1 - . Nation: China. USAF Sat Cat: 43011 . COSPAR: 2017-072B. Apogee: 811 km (503 mi). Perigee: 795 km (493 mi). Inclination: 98.70 deg. Period: 100.94 min. See HEAD 1 (Hede 1). ..

Xinyun - . Nation: China. USAF Sat Cat: 43012 . COSPAR: 2017-072C. Apogee: 797 km (495 mi). Perigee: 615 km (382 mi). Inclination: 98.67 deg. Period: 98.90 min.

2018 March 31 - . 03:21 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC9. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Gao Fen 1 02 xing - . Payload: gaofen yi hao 02 xing; GAOFEN 1-02. Nation: China. USAF Sat Cat: 43259 . COSPAR: 2018-031A. Apogee: 644 km (400 mi). Perigee: 637 km (395 mi). Inclination: 98.01 deg. Period: 97.53 min. See Gaofen 1-02 (GF 1-02). ..

Gao Fen 1 03 xing - . Payload: gaofen yi hao 03 xing; GAOFEN 1-03. Nation: China. USAF Sat Cat: 43260 . COSPAR: 2018-031B. Apogee: 645 km (400 mi). Perigee: 636 km (395 mi). Inclination: 98.01 deg. Period: 97.53 min. See Gaofen 1-03 (GF 1-03). ..

Gao Fen 1 04 xing - . Payload: gaofen yi hao 04 xing; GAOFEN 1-04. Nation: China. USAF Sat Cat: 43262 . COSPAR: 2018-031D. Apogee: 644 km (400 mi). Perigee: 637 km (395 mi). Inclination: 98.01 deg. Period: 97.53 min. See Gaofen 1-04 (GF 1-04). ..

2018 April 10 - . 04:24 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan Pad 43/94. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Yaogan 31 hao 01 zu 01 xing - . Payload: Jianbing-8 06-1; YAOGAN-31 A. Nation: China. USAF Sat Cat: 43275 . COSPAR: 2018-034A. Apogee: 1,116 km (693 mi). Perigee: 1,064 km (661 mi). Inclination: 63.41 deg. Period: 107.05 min. See Yaogan 31A (JB-8 6A). ..

Yaogan 31 hao 01 zu 02 xing - . Payload: Jianbing-8 06-2; YAOGAN-31 B. Nation: China. USAF Sat Cat: 43276 . COSPAR: 2018-034B. Apogee: 1,116 km (693 mi). Perigee: 1,064 km (661 mi). Inclination: 63.41 deg. Period: 107.05 min. See Yaogan 31B (JB-8 6B). ..

Yaogan 31 hao 01 zu 03 xing - . Payload: Jianbing-8 06-3; YAOGAN-31 C. Nation: China. USAF Sat Cat: 43277 . COSPAR: 2018-034C. Apogee: 1,116 km (693 mi). Perigee: 1,064 km (661 mi). Inclination: 63.41 deg. Period: 107.05 min. See Yaogan 31C (JB-8 6C). ..

Weina Jishu Shiyan Weixing - . Payload: Weina Jishu Shiyan Weixin; WEINA 1B. Nation: China. USAF Sat Cat: 43279 . COSPAR: 2018-034E. Apogee: 1,116 km (693 mi). Perigee: 1,064 km (661 mi). Inclination: 63.41 deg. Period: 107.05 min. See Weina 1B. ..

2018 May 8 - . 18:27 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC9. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Gao Fen 5 - . Payload: Gaofen wu hao weixing; GAOFEN-5. Nation: China. USAF Sat Cat: 43461 . COSPAR: 2018-043A. Apogee: 702 km (436 mi). Perigee: 699 km (434 mi). Inclination: 98.15 deg. Period: 98.78 min. See Gaofen 5 (GF 5). ..

2018 May 20 - . 21:27 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC3. LV Family: CZ. Launch Vehicle: Chang Zheng 4C.

Queqiao - . Payload: Chang'e-4 Relay. Nation: China. USAF Sat Cat: 43470 . COSPAR: 2018-045A. See Queqiao (Chang'e 4 Relay, CE 4 Relay). ..

Longjiang 1 - . Payload: DSLWP-A. Nation: China. USAF Sat Cat: 43471 . COSPAR: 2018-045B. See DSWLP A1 (Longjiang 1, LO 93, Lunar-OSCAR 93). ..

Longjiang 2 - . Payload: DSLWP-B. Nation: China. USAF Sat Cat: 43472 . COSPAR: 2018-045C. See DSWLP A2 (Longjiang 2, LO 94, Lunar-OSCAR 94). ..

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z