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, 14.5 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 GEESAT 4-02
1 65120U 25170B 26155.29163454 .00001949 00000-0 25901-3 0 9995
2 65120 49.9841 234.0776 0009405 37.3091 322.8499 14.83934121 44541Epoch: 2026-06-04T06:59Z
TLE epoch observation values (Epoch: 2026-06-04T06:59:57.224Z)
Latitude
-0°
Longitude
-123.64884°
Altitude
612.235 km
Speed
7.557 km/s
True Right ascension
15h 36m 18s
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
10:48:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
624.274 km
Perigee altitude
611.115 km
Semi-major axis
6,995.831 km
Eccentricity
0.00094
Inclination
49.9841°
RAAN
234.0776°
Arg. of periapsis
37.3091°
True anomaly
322.78475°
Mean anomaly
322.8499°
Eccentric anomaly
322.81733°
Mean motion
3.70923 °/min
Orbital period
97.06 mins
BSTAR
0.00025901
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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 | 2026-06-08 06:31:15.691Z | 209.151° SW | 2026-06-08 06:35:15.691Z | 118.181° SE | 35.362° | 2026-06-08 06:38:15.691Z | 68.865° E |
| 7 mins | 2026-06-08 08:13:15.691Z | 274.078° WNW | 2026-06-08 08:16:15.691Z | 337.707° N | 32.557° | 2026-06-08 08:20:15.691Z | 45.937° ENE |
| 5 mins | 2026-06-08 09:56:15.691Z | 318.473° NNW | 2026-06-08 09:58:15.691Z | 352.676° N | 20.797° | 2026-06-08 10:01:15.691Z | 42.297° NE |
| 6 mins | 2026-06-08 11:38:15.691Z | 326.836° NNW | 2026-06-08 11:41:15.691Z | 29.029° NE | 26.811° | 2026-06-08 11:44:15.691Z | 76.979° E |
| 7 mins | 2026-06-08 13:19:15.691Z | 300.548° NW | 2026-06-08 13:22:15.691Z | 258.852° W | 43.701° | 2026-06-08 13:26:15.691Z | 132.007° 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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