GEESAT 4-06, 65124
Orbit data source: Space-Track
GEESAT 4-06, 65124 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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65124 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, 0.9 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 4-06
1 65124U 25170F 26034.59262718 .00002969 00000-0 38087-3 0 9993
2 65124 49.9838 73.5159 0019853 252.1715 107.7058 14.83788503 26597Epoch: 2026-02-03T14:13Z
TLE epoch observation values (Epoch: 2026-02-03T14:13:22.988Z)
Latitude
0.00003°
Longitude
86.3988°
Altitude
622.182 km
Speed
7.547 km/s
True Right ascension
04h 54m 03s
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
08:35:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
632.042 km
Perigee altitude
604.262 km
Semi-major axis
6,996.289 km
Eccentricity
0.00199
Inclination
49.9838°
RAAN
73.5159°
Arg. of periapsis
252.1715°
True anomaly
107.92236°
Mean anomaly
107.7058°
Eccentric anomaly
107.8141°
Mean motion
3.70887 °/min
Orbital period
97.06 mins
BSTAR
0.00038087
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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 4-06 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 | 2026-02-04 06:38:16.132Z | 272.521° WNW | 2026-02-04 06:41:16.132Z | 339.362° N | 33.993° | 2026-02-04 06:45:16.132Z | 46.432° ENE |
| 5 mins | 2026-02-04 08:21:16.132Z | 318.194° NNW | 2026-02-04 08:23:16.132Z | 352.698° N | 21.506° | 2026-02-04 08:26:16.132Z | 41.848° NE |
| 6 mins | 2026-02-04 10:03:16.132Z | 326.932° NNW | 2026-02-04 10:06:16.132Z | 27.613° NE | 26.642° | 2026-02-04 10:09:16.132Z | 75.15° E |
| 7 mins | 2026-02-04 11:44:16.132Z | 302.126° NW | 2026-02-04 11:47:16.132Z | 278.486° WNW | 43.86° | 2026-02-04 11:51:16.132Z | 129.39° SE |
| 7 mins | 2026-02-05 05:13:16.132Z | 230.945° WSW | 2026-02-05 05:16:16.132Z | 81.574° E | 44.34° | 2026-02-05 05:20:16.132Z | 56.986° 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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