CHINASAT 6A, 37150
Orbit data source: Space-Track
CHINASAT 6A, 37150 is a payload satellite owned by China Satcom (CN) in GEO that was launched on Sat, 04 Sep 2010 UTC via a CHANG ZHENG 3B launch vehicle from the Xichang Space Center, China (XSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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37150 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Non-operational Commercial Communications
Bus & Motor
DFH-4, FY
Mass
5,100 kg wet, ~2,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 7.8 m
Radar Cross Section
19.960 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 CHINASAT 6A
1 37150U 10042A 26227.90749846 -.00000196 00000-0 00000-0 0 9996
2 37150 4.3753 76.4607 0000524 168.1173 331.5651 0.99696709 58471Epoch: 2026-08-15T21:46Z
TLE epoch observation values (Epoch: 2026-08-15T21:46:47.866Z)
Latitude
2.85412°
Longitude
-74.77693°
Altitude
35,945.822 km
Speed
3.069 km/s
True Right ascension
14h 24m 56s
True Declination
2° 51' 04"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
18:59:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,951.859 km
Perigee altitude
35,947.424 km
Semi-major axis
42,327.778 km
Eccentricity
0.00005
Inclination
4.3753°
RAAN
76.4607°
Arg. of periapsis
168.1173°
True anomaly
331.56224°
Mean anomaly
331.5651°
Eccentric anomaly
331.56367°
Mean motion
0.24923 °/min
Orbital period
1,444.43 mins
BSTAR
0
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Other satellites on launch #42 in the year 2010 (2010-09-04 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CHINASAT 6A Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2026-08-16 04:21:16.368Z | 140.859° SSE | 2026-08-16 18:43:16.368Z | 136.672° SSE | 32.464° | 2026-08-17 04:21:16.368Z | 143.184° SSE |
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37150 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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