GEESAT 4-09, 65127
Orbit data source: Space-Track
GEESAT 4-09, 65127 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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65127 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, 14.5 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 GEESAT 4-09
1 65127U 25170J 25331.73144590 .00000556 00000-0 15955-3 0 9997
2 65127 49.9941 43.6178 0021674 350.5411 9.5105 14.58056754 16302Epoch: 2025-11-27T17:33Z
TLE epoch observation values (Epoch: 2025-11-27T17:33:16.925Z)
Latitude
-0.00008°
Longitude
73.41307°
Altitude
684.865 km
Speed
7.523 km/s
True Right ascension
02h 54m 28s
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
04:35:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
715.548 km
Perigee altitude
684.865 km
Semi-major axis
7,078.343 km
Eccentricity
0.00217
Inclination
49.9941°
RAAN
43.6178°
Arg. of periapsis
350.5411°
True anomaly
9.55165°
Mean anomaly
9.5105°
Eccentric anomaly
9.53106°
Mean motion
3.64457 °/min
Orbital period
98.78 mins
BSTAR
0.00015955
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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 4-09 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-28 08:33:47.805Z | 248.464° W | 2025-11-28 08:37:47.805Z | 302.072° NW | 41.408° | 2025-11-28 08:42:47.805Z | 51.482° ENE |
| 6 mins | 2025-11-28 10:19:47.805Z | 308.347° NW | 2025-11-28 10:21:47.805Z | 342.981° N | 24.835° | 2025-11-28 10:25:47.805Z | 44.831° NE |
| 7 mins | 2025-11-28 12:03:47.805Z | 325.074° NNW | 2025-11-28 12:06:47.805Z | 18.318° NNE | 25.462° | 2025-11-28 12:10:47.805Z | 71.419° E |
| 8 mins | 2025-11-28 13:46:47.805Z | 310.048° NW | 2025-11-28 13:50:47.805Z | 66.596° ENE | 42.372° | 2025-11-28 13:54:47.805Z | 114.511° SE |
| 6 mins | 2025-11-28 15:30:47.805Z | 268.383° W | 2025-11-28 15:32:47.805Z | 237.375° WSW | 22.949° | 2025-11-28 15:36:47.805Z | 177.398° S |
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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