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
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: 15 hours ago
TLE from 15 hours ago
0 GEESAT 4-07
1 65125U 25170G 25283.40298409 .00003540 00000-0 41931-3 0 9993
2 65125 49.9916 252.8350 0017476 181.7001 178.3882 14.86665324 9334Epoch: 2025-10-10T09:40Z
TLE epoch observation values (Epoch: 2025-10-10T09:40:17.825Z)
Latitude
0°
Longitude
88.5114°
Altitude
621.112 km
Speed
7.543 km/s
True Right ascension
16h 51m 20s
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
19:15:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
621.335 km
Perigee altitude
596.913 km
Semi-major axis
6,987.261 km
Eccentricity
0.00175
Inclination
49.9916°
RAAN
252.835°
Arg. of periapsis
181.7001°
True anomaly
178.39382°
Mean anomaly
178.3882°
Eccentric anomaly
178.39101°
Mean motion
3.71606 °/min
Orbital period
96.88 mins
BSTAR
0.00041931
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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 | 2025-10-11 02:02:17.338Z | 263.506° W | 2025-10-11 02:05:17.338Z | 317.353° NNW | 35.64° | 2025-10-11 02:09:17.338Z | 45.239° ENE |
| 5 mins | 2025-10-11 03:45:17.338Z | 312.985° NW | 2025-10-11 03:47:17.338Z | 346.619° N | 21.174° | 2025-10-11 03:50:17.338Z | 38.267° NE |
| 6 mins | 2025-10-11 05:27:17.338Z | 326.818° NNW | 2025-10-11 05:30:17.338Z | 25.284° NE | 24.441° | 2025-10-11 05:33:17.338Z | 71.398° E |
| 7 mins | 2025-10-11 07:08:17.338Z | 306.06° NW | 2025-10-11 07:11:17.338Z | 338.962° N | 44.492° | 2025-10-11 07:15:17.338Z | 122.314° SE |
| 6 mins | 2025-10-12 00:35:17.338Z | 219.403° SW | 2025-10-12 00:38:17.338Z | 101.766° ESE | 41.539° | 2025-10-12 00:41:17.338Z | 61.72° 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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