GEESAT 6-02, 65714
Orbit data source: Space-Track
GEESAT 6-02, 65714 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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65714 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GEESAT 6-02
1 65714U 25214C 26170.61467412 .00001241 00000-0 17705-3 0 9995
2 65714 49.9858 297.2641 0010381 223.2024 136.8100 14.83374636 39867Epoch: 2026-06-19T14:45Z
TLE epoch observation values (Epoch: 2026-06-19T14:45:07.843Z)
Latitude
-0.00007°
Longitude
168.14024°
Altitude
624.534 km
Speed
7.545 km/s
True Right ascension
19h 49m 03s
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
07:13:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.717 km
Perigee altitude
612.189 km
Semi-major axis
6,997.59 km
Eccentricity
0.00104
Inclination
49.9858°
RAAN
297.2641°
Arg. of periapsis
223.2024°
True anomaly
136.89134°
Mean anomaly
136.81°
Eccentric anomaly
136.85068°
Mean motion
3.70784 °/min
Orbital period
97.09 mins
BSTAR
0.00017705
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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 6-02 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 10:34:26.403Z | 211.251° SW | 2026-06-21 10:38:26.403Z | 122.98° SE | 36.965° | 2026-06-21 10:42:26.403Z | 64.637° ENE |
| 7 mins | 2026-06-21 12:16:26.403Z | 273.707° WNW | 2026-06-21 12:19:26.403Z | 330.806° NNW | 32.273° | 2026-06-21 12:23:26.403Z | 44.508° NE |
| 6 mins | 2026-06-21 13:59:26.403Z | 315.653° NNW | 2026-06-21 14:01:26.403Z | 347.517° N | 20.85° | 2026-06-21 14:05:26.403Z | 49.447° ENE |
| 6 mins | 2026-06-21 15:41:26.403Z | 323.385° NNW | 2026-06-21 15:44:26.403Z | 20.651° NNE | 27.86° | 2026-06-21 15:47:26.403Z | 75.126° E |
| 7 mins | 2026-06-21 17:23:26.403Z | 298.001° NW | 2026-06-21 17:26:26.403Z | 176.472° S | 43.11° | 2026-06-21 17:30:26.403Z | 132.869° 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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