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, 14.5 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 GEESAT 4-09
1 65127U 25170J 26225.21582527 .00000519 00000-0 93762-4 0 9991
2 65127 49.9924 300.5372 0022425 249.0450 110.8088 14.81550520 54454Epoch: 2026-08-13T05:10Z
TLE epoch observation values (Epoch: 2026-08-13T05:10:47.303Z)
Latitude
0.00003°
Longitude
-98.81847°
Altitude
630.586 km
Speed
7.541 km/s
True Right ascension
20h 02m 08s
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
17:54:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.898 km
Perigee altitude
609.488 km
Semi-major axis
7,003.33 km
Eccentricity
0.00224
Inclination
49.9924°
RAAN
300.5372°
Arg. of periapsis
249.045°
True anomaly
111.04877°
Mean anomaly
110.8088°
Eccentric anomaly
110.92881°
Mean motion
3.70328 °/min
Orbital period
97.21 mins
BSTAR
0.000093762
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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 | 2026-08-14 07:14:45.329Z | 200.09° SSW | 2026-08-14 07:17:45.329Z | 147.774° SSE | 32.158° | 2026-08-14 07:21:45.329Z | 71.618° E |
| 7 mins | 2026-08-14 08:56:45.329Z | 269.059° W | 2026-08-14 08:59:45.329Z | 340.832° N | 35.813° | 2026-08-14 09:03:45.329Z | 47.252° ENE |
| 5 mins | 2026-08-14 10:39:45.329Z | 315.624° NNW | 2026-08-14 10:41:45.329Z | 349.851° N | 21.956° | 2026-08-14 10:44:45.329Z | 39.878° NE |
| 6 mins | 2026-08-14 12:21:45.329Z | 324.247° NNW | 2026-08-14 12:24:45.329Z | 19.63° NNE | 26.165° | 2026-08-14 12:27:45.329Z | 70.282° E |
| 7 mins | 2026-08-14 14:03:45.329Z | 304.679° NW | 2026-08-14 14:06:45.329Z | 116.835° SE | 44.83° | 2026-08-14 14:10:45.329Z | 125.071° 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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