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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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, 1.0 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 GEESAT 4-02
1 65120U 25170B 26289.27757665 .00001401 00000-0 19203-3 0 9995
2 65120 49.9872 332.4912 0009668 196.4504 163.6122 14.84352465 64448Epoch: 2026-10-16T06:39Z
TLE epoch observation values (Epoch: 2026-10-16T06:39:42.622Z)
Latitude
-0.00002°
Longitude
-152.2373°
Altitude
622.649 km
Speed
7.545 km/s
True Right ascension
22h 09m 57s
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
09:14:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
623.142 km
Perigee altitude
609.617 km
Semi-major axis
6,994.517 km
Eccentricity
0.00097
Inclination
49.9872°
RAAN
332.4912°
Arg. of periapsis
196.4504°
True anomaly
163.64342°
Mean anomaly
163.6122°
Eccentric anomaly
163.62781°
Mean motion
3.71028 °/min
Orbital period
97.03 mins
BSTAR
0.00019203
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-10-17 05:26:38.553Z | 212.963° SW | 2026-10-17 05:30:38.553Z | 140.842° SSE | 50.356° | 2026-10-17 05:34:38.553Z | 65.729° ENE |
| 6 mins | 2026-10-17 07:09:38.553Z | 280.308° WNW | 2026-10-17 07:11:38.553Z | 320.708° NNW | 37.765° | 2026-10-17 07:15:38.553Z | 42.34° NE |
| 5 mins | 2026-10-17 08:52:38.553Z | 325.903° NNW | 2026-10-17 08:54:38.553Z | 2.716° NNE | 22.467° | 2026-10-17 08:57:38.553Z | 47.089° ENE |
| 6 mins | 2026-10-17 10:34:38.553Z | 333.334° NNW | 2026-10-17 10:36:38.553Z | 15.88° NNE | 31.45° | 2026-10-17 10:40:38.553Z | 81.091° E |
| 7 mins | 2026-10-17 12:15:38.553Z | 298.944° NW | 2026-10-17 12:18:38.553Z | 184.137° SSW | 72.688° | 2026-10-17 12:22:38.553Z | 132.462° SE |
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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