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
Taizhou Xingkong
Mission
Operational spacecraft
Bus & Motor
GEESAT1, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.0 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 GEESAT 4-01
1 65119U 25170A 25283.43310222 .00003623 00000-0 42795-3 0 9998
2 65119 49.9912 253.0169 0020610 168.8851 191.2548 14.86684994 9345Epoch: 2025-10-10T10:23Z
TLE epoch observation values (Epoch: 2025-10-10T10:23:40.031Z)
Latitude
-0.00001°
Longitude
77.82108°
Altitude
622.968 km
Speed
7.541 km/s
True Right ascension
16h 52m 04s
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
19:03:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
623.463 km
Perigee altitude
594.662 km
Semi-major axis
6,987.2 km
Eccentricity
0.00206
Inclination
49.9912°
RAAN
253.0169°
Arg. of periapsis
168.8851°
True anomaly
191.20882°
Mean anomaly
191.2548°
Eccentric anomaly
191.2318°
Mean motion
3.71611 °/min
Orbital period
96.88 mins
BSTAR
0.00042795
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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 | 2025-10-11 01:06:06.914Z | 228.346° WSW | 2025-10-11 01:10:06.914Z | 86.583° E | 43.03° | 2025-10-11 01:14:06.914Z | 57.983° ENE |
| 6 mins | 2025-10-11 02:49:06.914Z | 297.608° NW | 2025-10-11 02:51:06.914Z | 340.161° N | 26.983° | 2025-10-11 02:55:06.914Z | 44.669° NE |
| 5 mins | 2025-10-11 04:31:06.914Z | 323.974° NNW | 2025-10-11 04:33:06.914Z | 357.866° N | 20.594° | 2025-10-11 04:36:06.914Z | 47.943° ENE |
| 6 mins | 2025-10-11 06:13:06.914Z | 327.705° NNW | 2025-10-11 06:15:06.914Z | 12.7° NNE | 32.06° | 2025-10-11 06:19:06.914Z | 91.241° ESE |
| 6 mins | 2025-10-11 07:54:06.914Z | 284.884° WNW | 2025-10-11 07:57:06.914Z | 201.051° SSW | 35.124° | 2025-10-11 08:00:06.914Z | 151.175° SSE |
| 5 mins | 2025-10-11 23:40:06.914Z | 171.808° S | 2025-10-11 23:42:06.914Z | 134.194° SE | 23.151° | 2025-10-11 23:45:06.914Z | 84.187° E |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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