GAOFEN 10R, 44622
Orbit data source: Space-Track
GAOFEN 10R, 44622 is a payload satellite owned by PLA SSF (CN) in SSO that was launched on Fri, 04 Oct 2019 UTC via a CHANG ZHENG 4C launch vehicle from the Taiyaun Space Center, China (TSC). 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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44622 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Operational Defense Imaging
Bus & Motor
CS-L3000B?, Unknown motor
Mass
~3,000 kg wet, ~3,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 3 Pan, Unknown HBR
Radar Cross Section
10.846 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 GAOFEN 10R
1 44622U 19066A 25309.94822096 .00002072 00000-0 26271-3 0 9991
2 44622 98.0217 257.3233 0008221 136.4179 223.7685 14.82821939329291Epoch: 2025-11-05T22:45Z
TLE epoch observation values (Epoch: 2025-11-05T22:45:26.290Z)
Latitude
-0.00004°
Longitude
-129.44981°
Altitude
627.61 km
Speed
7.542 km/s
True Right ascension
17h 09m 17s
True Declination
0° 00' 00"
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
05:50:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
623.224 km
Perigee altitude
611.722 km
Semi-major axis
6,995.61 km
Eccentricity
0.00082
Inclination
98.0217°
RAAN
257.3233°
Arg. of periapsis
136.4179°
True anomaly
223.70338°
Mean anomaly
223.7685°
Eccentric anomaly
223.73594°
Mean motion
3.70941 °/min
Orbital period
97.05 mins
BSTAR
0.00026271
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Other satellites on launch #66 in the year 2019 (2019-10-04 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.GAOFEN 10R 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-06 10:40:00.109Z | 327.788° NNW | 2025-11-06 10:42:00.109Z | 296.987° NW | 16.182° | 2025-11-06 10:44:00.109Z | 264.787° W |
| 5 mins | 2025-11-06 19:58:00.109Z | 116.556° SE | 2025-11-06 20:00:00.109Z | 74.138° E | 27.202° | 2025-11-06 20:03:00.109Z | 15.514° NNE |
| 5 mins | 2025-11-06 21:34:00.109Z | 225.965° WSW | 2025-11-06 21:36:00.109Z | 259.991° W | 20.078° | 2025-11-06 21:39:00.109Z | 310.299° NW |
| 7 mins | 2025-11-07 09:21:00.109Z | 22.682° NE | 2025-11-07 09:24:00.109Z | 121.888° SE | 42.232° | 2025-11-07 09:28:00.109Z | 184.532° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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