GEESAT 6-01, 65713
Orbit data source: Space-Track
GEESAT 6-01, 65713 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Wed, 24 Sep 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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65713 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, 1.1 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GEESAT 6-01
1 65713U 25214B 26170.61826809 .00001043 00000-0 15331-3 0 9996
2 65713 49.9870 297.3328 0012176 236.6224 123.3549 14.83340122 39868Epoch: 2026-06-19T14:50Z
TLE epoch observation values (Epoch: 2026-06-19T14:50:18.362Z)
Latitude
-0.00007°
Longitude
166.91157°
Altitude
624.035 km
Speed
7.545 km/s
True Right ascension
19h 49m 19s
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
08:33:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
628.081 km
Perigee altitude
611.041 km
Semi-major axis
6,997.698 km
Eccentricity
0.00122
Inclination
49.987°
RAAN
297.3328°
Arg. of periapsis
236.6224°
True anomaly
123.47135°
Mean anomaly
123.3549°
Eccentric anomaly
123.41313°
Mean motion
3.70775 °/min
Orbital period
97.09 mins
BSTAR
0.00015331
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Other satellites on launch #214 in the year 2025 (2025-09-24 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 6-01 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-21 10:39:10.860Z | 216.835° SW | 2026-06-21 10:43:10.860Z | 159.868° S | 38.619° | 2026-06-21 10:47:10.860Z | 65.667° ENE |
| 7 mins | 2026-06-21 12:22:10.860Z | 278.222° WNW | 2026-06-21 12:25:10.860Z | 340.118° N | 31.317° | 2026-06-21 12:29:10.860Z | 45.612° ENE |
| 5 mins | 2026-06-21 14:05:10.860Z | 319.443° NNW | 2026-06-21 14:07:10.860Z | 352.869° N | 21.062° | 2026-06-21 14:10:10.860Z | 42.839° NE |
| 6 mins | 2026-06-21 15:47:10.860Z | 325.537° NNW | 2026-06-21 15:50:10.860Z | 28.191° NE | 28.576° | 2026-06-21 15:53:10.860Z | 79.17° E |
| 7 mins | 2026-06-21 17:28:10.860Z | 297.924° NW | 2026-06-21 17:31:10.860Z | 251.929° W | 41.992° | 2026-06-21 17:35:10.860Z | 137.206° 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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