GEESAT 4-02, 65120
Orbit data source: Space-Track
GEESAT 4-02, 65120 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Fri, 08 Aug 2025 UTC via a JIELONG-3 launch vehicle from the Yellow Sea Launch Area, China (YSLA). 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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65120 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Taizhou Xingkong
Mission
Operational spacecraft
Bus & Motor
GEESAT1, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 GEESAT 4-02
1 65120U 25170B 25283.42601639 .00003664 00000-0 43363-3 0 9991
2 65120 49.9839 252.9427 0008475 207.7188 152.3301 14.86668136 9368Epoch: 2025-10-10T10:13Z
TLE epoch observation values (Epoch: 2025-10-10T10:13:27.816Z)
Latitude
0.00003°
Longitude
80.3048°
Altitude
614.143 km
Speed
7.551 km/s
True Right ascension
16h 51m 46s
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
19:06:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
615.038 km
Perigee altitude
603.195 km
Semi-major axis
6,987.254 km
Eccentricity
0.00085
Inclination
49.9839°
RAAN
252.9427°
Arg. of periapsis
207.7188°
True anomaly
152.37516°
Mean anomaly
152.3301°
Eccentric anomaly
152.35263°
Mean motion
3.71607 °/min
Orbital period
96.88 mins
BSTAR
0.00043363
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Other satellites on launch #170 in the year 2025 (2025-08-08 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.GEESAT 4-02 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 | 2025-10-11 00:55:33.238Z | 221.367° SW | 2025-10-11 00:58:33.238Z | 178.828° S | 41.135° | 2025-10-11 01:02:33.238Z | 62.237° ENE |
| 6 mins | 2025-10-11 02:37:33.238Z | 283.493° WNW | 2025-10-11 02:40:33.238Z | 342.963° N | 28.785° | 2025-10-11 02:43:33.238Z | 38.502° NE |
| 5 mins | 2025-10-11 04:20:33.238Z | 324.661° NNW | 2025-10-11 04:22:33.238Z | 359.79° N | 20.712° | 2025-10-11 04:25:33.238Z | 47.663° ENE |
| 6 mins | 2025-10-11 06:02:33.238Z | 330.84° NNW | 2025-10-11 06:04:33.238Z | 16.228° NNE | 30.327° | 2025-10-11 06:08:33.238Z | 87.492° E |
| 6 mins | 2025-10-11 07:43:33.238Z | 289.489° WNW | 2025-10-11 07:46:33.238Z | 191.512° SSW | 38.587° | 2025-10-11 07:49:33.238Z | 144.432° SSE |
| 5 mins | 2025-10-11 23:29:33.238Z | 166.51° S | 2025-10-11 23:31:33.238Z | 132.603° SE | 19.778° | 2025-10-11 23:34:33.238Z | 86.697° E |
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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