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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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: 8 hours ago
TLE from 8 hours ago
0 GEESAT 4-09
1 65127U 25170J 26255.90413497 .00001056 00000-0 16087-3 0 9990
2 65127 49.9912 158.7587 0022302 6.7798 353.3437 14.81629892 59006Epoch: 2026-09-12T21:41Z
TLE epoch observation values (Epoch: 2026-09-12T21:41:57.261Z)
Latitude
-0.00002°
Longitude
-158.63635°
Altitude
609.217 km
Speed
7.564 km/s
True Right ascension
10h 35m 02s
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
22:20:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.561 km
Perigee altitude
609.325 km
Semi-major axis
7,003.08 km
Eccentricity
0.00223
Inclination
49.9912°
RAAN
158.7587°
Arg. of periapsis
6.7798°
True anomaly
353.31399°
Mean anomaly
353.3437°
Eccentric anomaly
353.32886°
Mean motion
3.70348 °/min
Orbital period
97.21 mins
BSTAR
0.00016087
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-13 20:33:11.241Z | 229.769° WSW | 2026-09-13 20:36:11.241Z | 202.921° SW | 73.575° | 2026-09-13 20:40:11.241Z | 57.778° ENE |
| 6 mins | 2026-09-13 22:16:11.241Z | 296.402° NW | 2026-09-13 22:18:11.241Z | 335.995° NNW | 30.109° | 2026-09-13 22:22:11.241Z | 43.173° NE |
| 5 mins | 2026-09-13 23:59:11.241Z | 330.829° NNW | 2026-09-14 00:01:11.241Z | 7.39° NNE | 22.812° | 2026-09-14 00:04:11.241Z | 52.65° ENE |
| 7 mins | 2026-09-14 01:40:11.241Z | 319.132° NNW | 2026-09-14 01:43:11.241Z | 15.71° NNE | 41.228° | 2026-09-14 01:47:11.241Z | 92.609° ESE |
| 7 mins | 2026-09-14 03:22:11.241Z | 285.921° WNW | 2026-09-14 03:25:11.241Z | 214.334° SW | 45.764° | 2026-09-14 03:29:11.241Z | 149.882° 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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