GEESAT 4-07, 65125
Orbit data source: Space-Track
GEESAT 4-07, 65125 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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65125 intel report (Beta)
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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: 15 hours ago
TLE from 15 hours ago
0 GEESAT 4-07
1 65125U 25170G 26034.65010431 .00002979 00000-0 38230-3 0 9995
2 65125 49.9917 73.2837 0019173 265.4546 94.4202 14.83763545 26604Epoch: 2026-02-03T15:36Z
TLE epoch observation values (Epoch: 2026-02-03T15:36:09.012Z)
Latitude
-0.00002°
Longitude
65.41814°
Altitude
619.072 km
Speed
7.55 km/s
True Right ascension
04h 53m 08s
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
08:37:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
631.643 km
Perigee altitude
604.815 km
Semi-major axis
6,996.366 km
Eccentricity
0.00192
Inclination
49.9917°
RAAN
73.2837°
Arg. of periapsis
265.4546°
True anomaly
94.63921°
Mean anomaly
94.4202°
Eccentric anomaly
94.52971°
Mean motion
3.70881 °/min
Orbital period
97.07 mins
BSTAR
0.0003823
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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 4-07 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 | 2026-02-04 08:04:44.244Z | 298.75° NW | 2026-02-04 08:08:44.244Z | 359.672° N | 21.989° | 2026-02-04 08:11:44.244Z | 44.198° NE |
| 6 mins | 2026-02-04 09:48:44.244Z | 332.236° NNW | 2026-02-04 09:50:44.244Z | 10.817° NNE | 24.988° | 2026-02-04 09:54:44.244Z | 73.146° E |
| 7 mins | 2026-02-04 11:29:44.244Z | 307.625° NW | 2026-02-04 11:32:44.244Z | 22.846° NE | 44.531° | 2026-02-04 11:36:44.244Z | 120.275° SE |
| 5 mins | 2026-02-04 13:11:44.244Z | 260.932° W | 2026-02-04 13:13:44.244Z | 229.232° WSW | 18.007° | 2026-02-04 13:16:44.244Z | 186.254° SSW |
| 7 mins | 2026-02-05 04:57:44.244Z | 221.404° SW | 2026-02-05 05:00:44.244Z | 177.411° S | 41.478° | 2026-02-05 05:04:44.244Z | 62.099° 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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