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: 9 hours ago
TLE from 9 hours ago
0 GEESAT 4-09
1 65127U 25170J 26289.28916766 .00001325 00000-0 19439-3 0 9998
2 65127 49.9933 4.5085 0021789 135.5672 224.7018 14.81683071 63954Epoch: 2026-10-16T06:56Z
TLE epoch observation values (Epoch: 2026-10-16T06:56:24.085Z)
Latitude
-0.00003°
Longitude
-124.40419°
Altitude
635.42 km
Speed
7.536 km/s
True Right ascension
00h 18m 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
10:28:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.034 km
Perigee altitude
609.517 km
Semi-major axis
7,002.912 km
Eccentricity
0.00218
Inclination
49.9933°
RAAN
4.5085°
Arg. of periapsis
135.5672°
True anomaly
224.52651°
Mean anomaly
224.7018°
Eccentric anomaly
224.61412°
Mean motion
3.70361 °/min
Orbital period
97.2 mins
BSTAR
0.00019439
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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 | 2026-10-17 07:22:59.008Z | 204.233° SW | 2026-10-17 07:26:59.008Z | 121.283° SE | 40.697° | 2026-10-17 07:29:59.008Z | 71.526° E |
| 7 mins | 2026-10-17 09:04:59.008Z | 269.365° W | 2026-10-17 09:07:59.008Z | 331.454° NNW | 43.396° | 2026-10-17 09:11:59.008Z | 45.588° ENE |
| 6 mins | 2026-10-17 10:47:59.008Z | 313.738° NW | 2026-10-17 10:49:59.008Z | 346.016° N | 22.44° | 2026-10-17 10:53:59.008Z | 47.727° ENE |
| 5 mins | 2026-10-17 12:30:59.008Z | 334.392° NNW | 2026-10-17 12:32:59.008Z | 15.885° NNE | 29.062° | 2026-10-17 12:35:59.008Z | 69.86° E |
| 7 mins | 2026-10-17 14:11:59.008Z | 303.607° NW | 2026-10-17 14:14:59.008Z | 177.567° S | 86.771° | 2026-10-17 14:18:59.008Z | 126.792° SE |
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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