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: 8 hours ago
TLE from 8 hours ago
0 GEESAT 4-02
1 65120U 25170B 25331.97657809 .00002680 00000-0 35093-3 0 9993
2 65120 49.9865 27.0419 0010269 34.8234 325.3374 14.83316954 16583Epoch: 2025-11-27T23:26Z
TLE epoch observation values (Epoch: 2025-11-27T23:26:16.346Z)
Latitude
-0.00006°
Longitude
-31.65202°
Altitude
613.509 km
Speed
7.557 km/s
True Right ascension
01h 48m 10s
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
04:33:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.82 km
Perigee altitude
612.448 km
Semi-major axis
6,997.771 km
Eccentricity
0.00103
Inclination
49.9865°
RAAN
27.0419°
Arg. of periapsis
34.8234°
True anomaly
325.2704°
Mean anomaly
325.3374°
Eccentric anomaly
325.30391°
Mean motion
3.70769 °/min
Orbital period
97.1 mins
BSTAR
0.00035093
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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 | 2025-11-28 07:43:56.210Z | 254.12° W | 2025-11-28 07:47:56.210Z | 314.539° NW | 38.242° | 2025-11-28 07:51:56.210Z | 47.096° ENE |
| 6 mins | 2025-11-28 09:27:56.210Z | 308.922° NW | 2025-11-28 09:29:56.210Z | 342.163° N | 21.682° | 2025-11-28 09:33:56.210Z | 45.473° ENE |
| 5 mins | 2025-11-28 11:10:56.210Z | 334.721° NNW | 2025-11-28 11:12:56.210Z | 14.61° NNE | 23.969° | 2025-11-28 11:15:56.210Z | 64.824° ENE |
| 7 mins | 2025-11-28 12:51:56.210Z | 310.022° NW | 2025-11-28 12:54:56.210Z | 46.113° ENE | 43.715° | 2025-11-28 12:58:56.210Z | 117.233° SE |
| 5 mins | 2025-11-28 14:33:56.210Z | 260.991° W | 2025-11-28 14:35:56.210Z | 226.964° WSW | 19.505° | 2025-11-28 14:38:56.210Z | 182.647° SSW |
| 7 mins | 2025-11-29 06:20:56.210Z | 214.735° SW | 2025-11-29 06:23:56.210Z | 122.346° SE | 40.614° | 2025-11-29 06:27:56.210Z | 61.929° ENE |
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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