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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GEESAT 4-07
1 65125U 25170G 26225.16110242 .00000476 00000-0 83458-4 0 9997
2 65125 49.9921 269.9674 0018468 272.6461 87.2364 14.84211226 54890Epoch: 2026-08-13T03:51Z
TLE epoch observation values (Epoch: 2026-08-13T03:51:59.249Z)
Latitude
0.00004°
Longitude
-109.6341°
Altitude
616.007 km
Speed
7.553 km/s
True Right ascension
17h 59m 52s
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
17:54:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
629.741 km
Perigee altitude
603.904 km
Semi-major axis
6,994.96 km
Eccentricity
0.00185
Inclination
49.9921°
RAAN
269.9674°
Arg. of periapsis
272.6461°
True anomaly
87.4478°
Mean anomaly
87.2364°
Eccentric anomaly
87.3421°
Mean motion
3.70993 °/min
Orbital period
97.04 mins
BSTAR
0.000083458
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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 | 2026-08-14 05:55:11.431Z | 227.825° WSW | 2026-08-14 05:58:11.431Z | 129.251° SE | 44.443° | 2026-08-14 06:02:11.431Z | 58.141° ENE |
| 6 mins | 2026-08-14 07:37:11.431Z | 290.863° WNW | 2026-08-14 07:40:11.431Z | 351.574° N | 27.102° | 2026-08-14 07:43:11.431Z | 40.345° NE |
| 5 mins | 2026-08-14 09:20:11.431Z | 327.262° NNW | 2026-08-14 09:22:11.431Z | 2.598° NNE | 21.386° | 2026-08-14 09:25:11.431Z | 50.291° ENE |
| 7 mins | 2026-08-14 11:01:11.431Z | 318.673° NNW | 2026-08-14 11:04:11.431Z | 13.582° NNE | 33.013° | 2026-08-14 11:08:11.431Z | 91.718° ESE |
| 7 mins | 2026-08-14 12:43:11.431Z | 285.591° WNW | 2026-08-14 12:46:11.431Z | 209.005° SW | 35.795° | 2026-08-14 12:50:11.431Z | 148.484° SSE |
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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