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: 16 hours ago
TLE from 16 hours ago
0 GEESAT 4-02
1 65120U 25170B 26034.60361790 .00002792 00000-0 36050-3 0 9993
2 65120 49.9852 73.6144 0010789 295.7423 64.2402 14.83777374 26620Epoch: 2026-02-03T14:29Z
TLE epoch observation values (Epoch: 2026-02-03T14:29:12.586Z)
Latitude
0.00004°
Longitude
82.52981°
Altitude
614.695 km
Speed
7.555 km/s
True Right ascension
04h 54m 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
08:38:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
625.735 km
Perigee altitude
610.639 km
Semi-major axis
6,996.324 km
Eccentricity
0.00108
Inclination
49.9852°
RAAN
73.6144°
Arg. of periapsis
295.7423°
True anomaly
64.35161°
Mean anomaly
64.2402°
Eccentric anomaly
64.2959°
Mean motion
3.70884 °/min
Orbital period
97.07 mins
BSTAR
0.0003605
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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 | 2026-02-04 06:53:51.411Z | 272.935° WNW | 2026-02-04 06:57:51.411Z | 342.312° N | 30.391° | 2026-02-04 07:01:51.411Z | 45.789° ENE |
| 5 mins | 2026-02-04 08:37:51.411Z | 321.104° NNW | 2026-02-04 08:39:51.411Z | 355.005° N | 21.007° | 2026-02-04 08:42:51.411Z | 44.353° NE |
| 6 mins | 2026-02-04 10:19:51.411Z | 326.539° NNW | 2026-02-04 10:22:51.411Z | 32.495° NE | 29.06° | 2026-02-04 10:25:51.411Z | 81.672° E |
| 7 mins | 2026-02-04 12:00:51.411Z | 295.948° NW | 2026-02-04 12:03:51.411Z | 235.196° WSW | 41.706° | 2026-02-04 12:07:51.411Z | 139.231° SSE |
| 5 mins | 2026-02-05 03:48:51.411Z | 171.603° S | 2026-02-05 03:51:51.411Z | 125.064° SE | 18.368° | 2026-02-05 03:53:51.411Z | 94.469° ESE |
| 7 mins | 2026-02-05 05:29:51.411Z | 243.701° WSW | 2026-02-05 05:32:51.411Z | 15.47° NNE | 43.381° | 2026-02-05 05:36:51.411Z | 53.678° 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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