GEESAT 4-04, 65122
Orbit data source: Space-Track
GEESAT 4-04, 65122 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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65122 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: 17 hours ago
TLE from 17 hours ago
0 GEESAT 4-04
1 65122U 25170D 26034.58846693 .00043720 00000-0 97162-3 0 9999
2 65122 49.9847 41.4385 0005178 92.6329 267.5227 15.43181450 27020Epoch: 2026-02-03T14:07Z
TLE epoch observation values (Epoch: 2026-02-03T14:07:23.542Z)
Latitude
-0.00002°
Longitude
55.82315°
Altitude
437.438 km
Speed
7.651 km/s
True Right ascension
02h 45m 45s
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
08:41:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.037 km
Perigee altitude
433.978 km
Semi-major axis
6,815.645 km
Eccentricity
0.00052
Inclination
49.9847°
RAAN
41.4385°
Arg. of periapsis
92.6329°
True anomaly
267.46342°
Mean anomaly
267.5227°
Eccentric anomaly
267.49306°
Mean motion
3.85729 °/min
Orbital period
93.33 mins
BSTAR
0.00097162
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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 4-04 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-04 07:37:58.207Z | 337.624° N | 2026-02-04 07:39:58.207Z | 21.273° NNE | 17.76° | 2026-02-04 07:41:58.207Z | 58.607° ENE |
| 4 mins | 2026-02-04 09:15:58.207Z | 318.4° NNW | 2026-02-04 09:16:58.207Z | 344.322° N | 39.525° | 2026-02-04 09:19:58.207Z | 112.368° ESE |
| 5 mins | 2026-02-05 03:38:58.207Z | 260.59° W | 2026-02-05 03:40:58.207Z | 322.92° NNW | 37.569° | 2026-02-05 03:43:58.207Z | 45.754° 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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