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
GWCG
Mission
Operational Commercial Navigation
Bus & Motor
GPS100, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 GEESAT 4-02
1 65120U 25170B 26035.14239440 .00002710 00000-0 35068-3 0 9997
2 65120 49.9852 71.1162 0010783 297.7543 62.2301 14.83780585 26705Epoch: 2026-02-04T03:25Z
TLE epoch observation values (Epoch: 2026-02-04T03:25:02.876Z)
Latitude
-0.00003°
Longitude
-114.45903°
Altitude
614.45 km
Speed
7.555 km/s
True Right ascension
04h 44m 27s
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
10:15:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
625.721 km
Perigee altitude
610.633 km
Semi-major axis
6,996.314 km
Eccentricity
0.00108
Inclination
49.9852°
RAAN
71.1162°
Arg. of periapsis
297.7543°
True anomaly
62.3395°
Mean anomaly
62.2301°
Eccentric anomaly
62.28479°
Mean motion
3.70885 °/min
Orbital period
97.07 mins
BSTAR
0.00035068
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-04 08:36:57.580Z | 311.11° NW | 2026-02-04 08:39:57.580Z | 357.078° N | 21.056° | 2026-02-04 08:42:57.580Z | 45.439° ENE |
| 6 mins | 2026-02-04 10:19:57.580Z | 327.704° NNW | 2026-02-04 10:21:57.580Z | 6.339° NNE | 28.918° | 2026-02-04 10:25:57.580Z | 82.433° E |
| 7 mins | 2026-02-04 12:00:57.580Z | 295.57° NW | 2026-02-04 12:03:57.580Z | 227.105° WSW | 41.893° | 2026-02-04 12:07:57.580Z | 138.969° SSE |
| 5 mins | 2026-02-05 03:48:57.580Z | 170.479° S | 2026-02-05 03:51:57.580Z | 123.212° SE | 18.276° | 2026-02-05 03:53:57.580Z | 93.271° ESE |
| 7 mins | 2026-02-05 05:29:57.580Z | 244.003° WSW | 2026-02-05 05:32:57.580Z | 22.357° NNE | 42.84° | 2026-02-05 05:36:57.580Z | 53.799° ENE |
| 6 mins | 2026-02-05 07:11:57.580Z | 300.802° NW | 2026-02-05 07:13:57.580Z | 336.009° NNW | 24.187° | 2026-02-05 07:17:57.580Z | 42.826° NE |
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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