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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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: 9 hours ago
TLE from 9 hours ago
0 GEESAT 4-07
1 65125U 25170G 26095.94123009 .00002551 00000-0 33142-3 0 9993
2 65125 49.9901 149.2077 0017956 137.5786 222.6544 14.83778400 35700Epoch: 2026-04-05T22:35Z
TLE epoch observation values (Epoch: 2026-04-05T22:35:22.279Z)
Latitude
-0.00001°
Longitude
-23.87457°
Altitude
627.214 km
Speed
7.541 km/s
True Right ascension
09h 56m 49s
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
13:39:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.745 km
Perigee altitude
605.62 km
Semi-major axis
6,996.32 km
Eccentricity
0.0018
Inclination
49.9901°
RAAN
149.2077°
Arg. of periapsis
137.5786°
True anomaly
222.51521°
Mean anomaly
222.6544°
Eccentric anomaly
222.58478°
Mean motion
3.70885 °/min
Orbital period
97.07 mins
BSTAR
0.00033142
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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 | 2026-04-06 08:34:23.837Z | 290.26° WNW | 2026-04-06 08:37:23.837Z | 338.977° N | 24.795° | 2026-04-06 08:41:23.837Z | 43.993° NE |
| 5 mins | 2026-04-06 10:18:23.837Z | 334.714° NNW | 2026-04-06 10:20:23.837Z | 13.015° NNE | 21.147° | 2026-04-06 10:23:23.837Z | 57.524° ENE |
| 7 mins | 2026-04-06 11:59:23.837Z | 319.618° NNW | 2026-04-06 12:02:23.837Z | 33.992° NE | 36.112° | 2026-04-06 12:06:23.837Z | 100.826° ESE |
| 6 mins | 2026-04-06 13:41:23.837Z | 273.332° WNW | 2026-04-06 13:43:23.837Z | 227.659° WSW | 30.137° | 2026-04-06 13:47:23.837Z | 158.545° S |
| 6 mins | 2026-04-07 05:28:23.837Z | 189.159° SSW | 2026-04-07 05:31:23.837Z | 123.125° SE | 28.909° | 2026-04-07 05:34:23.837Z | 75.118° E |
| 7 mins | 2026-04-07 07:09:23.837Z | 264.892° W | 2026-04-07 07:12:23.837Z | 340.612° N | 37.038° | 2026-04-07 07:16:23.837Z | 48.133° ENE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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