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: 5 days ago
TLE from 5 days ago
0 GEESAT 4-09
1 65127U 25170J 26030.69625674 .00001191 00000-0 24054-3 0 9992
2 65127 49.9943 118.4430 0025935 244.3084 115.5169 14.67830623 25635Epoch: 2026-01-30T16:42Z
TLE epoch observation values (Epoch: 2026-01-30T16:42:36.582Z)
Latitude
-0.00001°
Longitude
97.85967°
Altitude
676.452 km
Speed
7.516 km/s
True Right ascension
07h 53m 46s
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
08:39:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
687.032 km
Perigee altitude
650.48 km
Semi-major axis
7,046.893 km
Eccentricity
0.00259
Inclination
49.9943°
RAAN
118.443°
Arg. of periapsis
244.3084°
True anomaly
115.78473°
Mean anomaly
115.5169°
Eccentric anomaly
115.65085°
Mean motion
3.66899 °/min
Orbital period
98.12 mins
BSTAR
0.00024054
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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 | 2026-02-04 08:01:39.617Z | 253.163° W | 2026-02-04 08:05:39.617Z | 311.633° NW | 39.639° | 2026-02-04 08:10:39.617Z | 50.437° ENE |
| 6 mins | 2026-02-04 09:46:39.617Z | 306.898° NW | 2026-02-04 09:49:39.617Z | 358.849° N | 23.885° | 2026-02-04 09:52:39.617Z | 43.137° NE |
| 6 mins | 2026-02-04 11:30:39.617Z | 330.136° NNW | 2026-02-04 11:32:39.617Z | 6.136° NNE | 25.725° | 2026-02-04 11:36:39.617Z | 69.717° E |
| 8 mins | 2026-02-04 13:12:39.617Z | 308.474° NW | 2026-02-04 13:15:39.617Z | 345.759° N | 43.191° | 2026-02-04 13:20:39.617Z | 118.483° SE |
| 6 mins | 2026-02-04 14:55:39.617Z | 267.892° W | 2026-02-04 14:58:39.617Z | 220.682° SW | 20.224° | 2026-02-04 15:01:39.617Z | 180.908° SSW |
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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