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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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, 1.0 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 GEESAT 4-01
1 65119U 25170A 25331.98853573 .00002899 00000-0 37836-3 0 9997
2 65119 49.9887 27.1394 0011108 356.7910 3.2955 14.83193473 16562Epoch: 2025-11-27T23:43Z
TLE epoch observation values (Epoch: 2025-11-27T23:43:29.487Z)
Latitude
-0°
Longitude
-35.87101°
Altitude
612.045 km
Speed
7.559 km/s
True Right ascension
01h 48m 33s
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
04:32:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.796 km
Perigee altitude
612.248 km
Semi-major axis
6,998.159 km
Eccentricity
0.00111
Inclination
49.9887°
RAAN
27.1394°
Arg. of periapsis
356.791°
True anomaly
3.30283°
Mean anomaly
3.2955°
Eccentric anomaly
3.29916°
Mean motion
3.70738 °/min
Orbital period
97.1 mins
BSTAR
0.00037836
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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 | 2025-11-28 08:02:46.318Z | 266.009° W | 2025-11-28 08:06:46.318Z | 351.628° N | 33.814° | 2025-11-28 08:09:46.318Z | 43.131° NE |
| 5 mins | 2025-11-28 09:46:46.318Z | 321.843° NNW | 2025-11-28 09:48:46.318Z | 358.731° N | 21.253° | 2025-11-28 09:51:46.318Z | 44.651° NE |
| 6 mins | 2025-11-28 11:28:46.318Z | 330.422° NNW | 2025-11-28 11:30:46.318Z | 8.943° NNE | 26.094° | 2025-11-28 11:34:46.318Z | 76.206° E |
| 7 mins | 2025-11-28 13:09:46.318Z | 303.207° NW | 2025-11-28 13:12:46.318Z | 271.838° WNW | 44.824° | 2025-11-28 13:16:46.318Z | 127.209° SE |
| 7 mins | 2025-11-29 06:38:46.318Z | 229.15° WSW | 2025-11-29 06:41:46.318Z | 143.785° SSE | 44.632° | 2025-11-29 06:45:46.318Z | 57.78° 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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