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: 4 days ago
TLE from 4 days ago
0 GEESAT 4-01
1 65119U 25170A 26155.30259521 .00002029 00000-0 26846-3 0 9995
2 65119 49.9868 234.2157 0010138 358.5624 1.5284 14.83935624 44528Epoch: 2026-06-04T07:15Z
TLE epoch observation values (Epoch: 2026-06-04T07:15:44.226Z)
Latitude
0.00003°
Longitude
-127.46735°
Altitude
610.383 km
Speed
7.559 km/s
True Right ascension
15h 36m 51s
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
10:50:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
624.782 km
Perigee altitude
610.597 km
Semi-major axis
6,995.826 km
Eccentricity
0.00101
Inclination
49.9868°
RAAN
234.2157°
Arg. of periapsis
358.5624°
True anomaly
1.5315°
Mean anomaly
1.5284°
Eccentric anomaly
1.52995°
Mean motion
3.70924 °/min
Orbital period
97.05 mins
BSTAR
0.00026846
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-08 06:47:05.592Z | 220.953° SW | 2026-06-08 06:51:05.592Z | 149.292° SSE | 41.503° | 2026-06-08 06:55:05.592Z | 62.287° ENE |
| 6 mins | 2026-06-08 08:30:05.592Z | 284.244° WNW | 2026-06-08 08:33:05.592Z | 348.799° N | 29.118° | 2026-06-08 08:36:05.592Z | 40.395° NE |
| 5 mins | 2026-06-08 10:13:05.592Z | 324.622° NNW | 2026-06-08 10:15:05.592Z | 359.979° N | 20.809° | 2026-06-08 10:18:05.592Z | 47.402° ENE |
| 6 mins | 2026-06-08 11:55:05.592Z | 329.031° NNW | 2026-06-08 11:57:05.592Z | 10.8° NNE | 29.77° | 2026-06-08 12:01:05.592Z | 85.218° E |
| 7 mins | 2026-06-08 13:36:05.592Z | 292.987° NW | 2026-06-08 13:39:05.592Z | 212.487° SW | 40.699° | 2026-06-08 13:43:05.592Z | 140.918° 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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