GEESAT 6-05, 65717
Orbit data source: Space-Track
GEESAT 6-05, 65717 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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65717 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: 13 hours ago
TLE from 13 hours ago
0 GEESAT 6-05
1 65717U 25214F 26171.34854877 .00001116 00000-0 16201-3 0 9995
2 65717 49.9826 293.6857 0012990 223.9326 136.0580 14.83379218 39971Epoch: 2026-06-20T08:21Z
TLE epoch observation values (Epoch: 2026-06-20T08:21:54.613Z)
Latitude
-0.00003°
Longitude
-100.35634°
Altitude
625.77 km
Speed
7.544 km/s
True Right ascension
19h 34m 44s
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
08:32:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
628.529 km
Perigee altitude
610.349 km
Semi-major axis
6,997.576 km
Eccentricity
0.0013
Inclination
49.9826°
RAAN
293.6857°
Arg. of periapsis
223.9326°
True anomaly
136.16117°
Mean anomaly
136.058°
Eccentric anomaly
136.1096°
Mean motion
3.70785 °/min
Orbital period
97.09 mins
BSTAR
0.00016201
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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 6-05 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 10:23:38.114Z | 205.658° SW | 2026-06-21 10:27:38.114Z | 129.696° SE | 33.671° | 2026-06-21 10:31:38.114Z | 67.698° E |
| 7 mins | 2026-06-21 12:05:38.114Z | 268.454° W | 2026-06-21 12:08:38.114Z | 326.633° NNW | 34.517° | 2026-06-21 12:12:38.114Z | 45.15° ENE |
| 6 mins | 2026-06-21 13:48:38.114Z | 313.452° NW | 2026-06-21 13:50:38.114Z | 345.679° N | 21.182° | 2026-06-21 13:54:38.114Z | 47.816° ENE |
| 6 mins | 2026-06-21 15:30:38.114Z | 323.259° NNW | 2026-06-21 15:33:38.114Z | 18.172° NNE | 26.373° | 2026-06-21 15:36:38.114Z | 71.046° E |
| 7 mins | 2026-06-21 17:12:38.114Z | 302.934° NW | 2026-06-21 17:15:38.114Z | 146.771° SSE | 44.528° | 2026-06-21 17:19:38.114Z | 127.262° 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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