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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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: 10 hours ago
TLE from 10 hours ago
0 GAOFEN 10R
1 44622U 19066A 26049.87531375 .00001435 00000-0 18295-3 0 9991
2 44622 98.0369 2.6959 0007023 159.7768 200.3725 14.83080773344844Epoch: 2026-02-18T21:00Z
TLE epoch observation values (Epoch: 2026-02-18T21:00:27.108Z)
Latitude
0.00004°
Longitude
-101.25174°
Altitude
627.247 km
Speed
7.542 km/s
True Right ascension
00h 10m 47s
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
09:58:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
621.572 km
Perigee altitude
611.747 km
Semi-major axis
6,994.796 km
Eccentricity
0.0007
Inclination
98.0369°
RAAN
2.6959°
Arg. of periapsis
159.7768°
True anomaly
200.34451°
Mean anomaly
200.3725°
Eccentric anomaly
200.3585°
Mean motion
3.71006 °/min
Orbital period
97.03 mins
BSTAR
0.00018295
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-19 08:55:06.329Z | 38.531° NE | 2026-02-19 08:58:06.329Z | 84.698° E | 24.448° | 2026-02-19 09:02:06.329Z | 154.759° SSE |
| 4 mins | 2026-02-19 10:33:06.329Z | 321.041° NNW | 2026-02-19 10:34:06.329Z | 301.19° NW | 21.9° | 2026-02-19 10:37:06.329Z | 246.211° WSW |
| 4 mins | 2026-02-19 19:51:06.329Z | 92.254° ESE | 2026-02-19 19:52:06.329Z | 73.299° E | 20.172° | 2026-02-19 19:55:06.329Z | 23.025° NE |
| 6 mins | 2026-02-19 21:26:06.329Z | 214.975° SW | 2026-02-19 21:28:06.329Z | 257.826° W | 27.628° | 2026-02-19 21:32:06.329Z | 326.263° NNW |
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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