GEESAT 4-01, 65119
Orbit data source: Space-Track
GEESAT 4-01, 65119 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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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, 1.0 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 GEESAT 4-01
1 65119U 25170A 26289.28974103 .00001445 00000-0 19725-3 0 9999
2 65119 49.9897 332.6698 0010183 158.7976 201.3387 14.84346216 64422Epoch: 2026-10-16T06:57Z
TLE epoch observation values (Epoch: 2026-10-16T06:57:13.624Z)
Latitude
0.00001°
Longitude
-156.44984°
Altitude
622.816 km
Speed
7.545 km/s
True Right ascension
22h 10m 40s
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
09:11:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
623.521 km
Perigee altitude
609.276 km
Semi-major axis
6,994.536 km
Eccentricity
0.00102
Inclination
49.9897°
RAAN
332.6698°
Arg. of periapsis
158.7976°
True anomaly
201.29629°
Mean anomaly
201.3387°
Eccentric anomaly
201.31749°
Mean motion
3.71026 °/min
Orbital period
97.03 mins
BSTAR
0.00019725
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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 4-01 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 | 2026-10-17 05:45:56.859Z | 220.56° SW | 2026-10-17 05:48:56.859Z | 136.686° SSE | 67.774° | 2026-10-17 05:52:56.859Z | 60.572° ENE |
| 6 mins | 2026-10-17 07:27:56.859Z | 287.795° WNW | 2026-10-17 07:30:56.859Z | 352.78° N | 32.401° | 2026-10-17 07:33:56.859Z | 40.965° NE |
| 5 mins | 2026-10-17 09:10:56.859Z | 327.514° NNW | 2026-10-17 09:12:56.859Z | 3.467° NNE | 22.271° | 2026-10-17 09:15:56.859Z | 49.316° ENE |
| 7 mins | 2026-10-17 10:51:56.859Z | 320.733° NNW | 2026-10-17 10:54:56.859Z | 16.739° NNE | 36.132° | 2026-10-17 10:58:56.859Z | 87.744° E |
| 7 mins | 2026-10-17 12:33:56.859Z | 290.246° WNW | 2026-10-17 12:36:56.859Z | 199.781° SSW | 54.265° | 2026-10-17 12:40:56.859Z | 142.202° SSE |
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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