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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 GEESAT 4-01
1 65119U 25170A 26095.83804130 .00002707 00000-0 34981-3 0 9990
2 65119 49.9863 149.9320 0010103 132.4013 227.7782 14.83851184 35691Epoch: 2026-04-05T20:06Z
TLE epoch observation values (Epoch: 2026-04-05T20:06:46.768Z)
Latitude
0.00002°
Longitude
14.09942°
Altitude
622.49 km
Speed
7.546 km/s
True Right ascension
09h 59m 43s
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
11:43:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
625.023 km
Perigee altitude
610.887 km
Semi-major axis
6,996.092 km
Eccentricity
0.00101
Inclination
49.9863°
RAAN
149.932°
Arg. of periapsis
132.4013°
True anomaly
227.69254°
Mean anomaly
227.7782°
Eccentric anomaly
227.73536°
Mean motion
3.70903 °/min
Orbital period
97.06 mins
BSTAR
0.00034981
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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 | 2026-04-06 05:58:35.518Z | 200.758° SSW | 2026-04-06 06:01:35.518Z | 147.651° SSE | 32.023° | 2026-04-06 06:05:35.518Z | 71.101° E |
| 6 mins | 2026-04-06 07:40:35.518Z | 271.038° WNW | 2026-04-06 07:43:35.518Z | 348.83° N | 34.732° | 2026-04-06 07:46:35.518Z | 43.093° NE |
| 5 mins | 2026-04-06 09:23:35.518Z | 320.873° NNW | 2026-04-06 09:25:35.518Z | 357.923° N | 21.193° | 2026-04-06 09:28:35.518Z | 44.12° NE |
| 6 mins | 2026-04-06 11:05:35.518Z | 330.831° NNW | 2026-04-06 11:07:35.518Z | 9.473° NNE | 25.403° | 2026-04-06 11:11:35.518Z | 75.416° E |
| 7 mins | 2026-04-06 12:46:35.518Z | 304.459° NW | 2026-04-06 12:49:35.518Z | 316.577° NNW | 44.975° | 2026-04-06 12:53:35.518Z | 125.196° SE |
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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