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: 4 days ago
TLE from 4 days ago
0 GEESAT 4-04
1 65122U 25170D 25328.42610881 .00014636 00000-0 79699-3 0 9994
2 65122 49.9817 41.4912 0011680 96.8624 263.3656 15.14531646 16057Epoch: 2025-11-24T10:13Z
TLE epoch observation values (Epoch: 2025-11-24T10:13:35.801Z)
Latitude
-0.00003°
Longitude
-175.53424°
Altitude
523.891 km
Speed
7.602 km/s
True Right ascension
02h 45m 57s
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
531.233 km
Perigee altitude
515.112 km
Semi-major axis
6,901.309 km
Eccentricity
0.00117
Inclination
49.9817°
RAAN
41.4912°
Arg. of periapsis
96.8624°
True anomaly
263.23268°
Mean anomaly
263.3656°
Eccentric anomaly
263.29914°
Mean motion
3.7857 °/min
Orbital period
95.09 mins
BSTAR
0.00079699
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-28 07:52:56.561Z | 267.253° W | 2025-11-28 07:55:56.561Z | 317.692° NNW | 30.498° | 2025-11-28 07:59:56.561Z | 44.099° NE |
| 4 mins | 2025-11-28 09:34:56.561Z | 326.56° NNW | 2025-11-28 09:35:56.561Z | 345.153° N | 17.674° | 2025-11-28 09:38:56.561Z | 38.482° NE |
| 4 mins | 2025-11-28 11:14:56.561Z | 338.38° N | 2025-11-28 11:16:56.561Z | 23.753° NE | 22.393° | 2025-11-28 11:18:56.561Z | 62.488° ENE |
| 6 mins | 2025-11-28 12:53:56.561Z | 305.148° NW | 2025-11-28 12:55:56.561Z | 311.548° NW | 43.878° | 2025-11-28 12:59:56.561Z | 124.487° SE |
| 6 mins | 2025-11-29 05:59:56.561Z | 206.824° SW | 2025-11-29 06:02:56.561Z | 116.42° SE | 35.064° | 2025-11-29 06:05:56.561Z | 66.989° 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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