GEESAT 6-07, 65719
Orbit data source: Space-Track
GEESAT 6-07, 65719 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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65719 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 6-07
1 65719U 25214H 26171.37810297 .00001205 00000-0 17265-3 0 9998
2 65719 49.9817 293.1398 0010096 245.8756 114.1127 14.83385491 39999Epoch: 2026-06-20T09:04Z
TLE epoch observation values (Epoch: 2026-06-20T09:04:28.096Z)
Latitude
0.00002°
Longitude
-111.57084°
Altitude
622.092 km
Speed
7.547 km/s
True Right ascension
19h 32m 33s
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
08:32:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.484 km
Perigee altitude
612.355 km
Semi-major axis
6,997.556 km
Eccentricity
0.00101
Inclination
49.9817°
RAAN
293.1398°
Arg. of periapsis
245.8756°
True anomaly
114.21824°
Mean anomaly
114.1127°
Eccentric anomaly
114.16548°
Mean motion
3.70786 °/min
Orbital period
97.09 mins
BSTAR
0.00017265
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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 6-07 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 09:29:00.926Z | 158.013° S | 2026-06-21 09:31:00.926Z | 128.654° SE | 15.434° | 2026-06-21 09:33:00.926Z | 99.737° ESE |
| 7 mins | 2026-06-21 11:09:00.926Z | 234.508° WSW | 2026-06-21 11:12:00.926Z | 58.14° ENE | 44.814° | 2026-06-21 11:16:00.926Z | 55.965° ENE |
| 6 mins | 2026-06-21 12:51:00.926Z | 293.883° NW | 2026-06-21 12:54:00.926Z | 351.867° N | 25.849° | 2026-06-21 12:57:00.926Z | 40.254° NE |
| 5 mins | 2026-06-21 14:34:00.926Z | 327.202° NNW | 2026-06-21 14:36:00.926Z | 2.114° NNE | 21.553° | 2026-06-21 14:39:00.926Z | 51.421° ENE |
| 6 mins | 2026-06-21 16:16:00.926Z | 324.881° NNW | 2026-06-21 16:18:00.926Z | 9.475° NNE | 34.709° | 2026-06-21 16:22:00.926Z | 95.481° ESE |
| 6 mins | 2026-06-21 17:57:00.926Z | 282.518° WNW | 2026-06-21 18:00:00.926Z | 215.307° SW | 32.469° | 2026-06-21 18:03:00.926Z | 159.618° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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