GEESAT 5-07, 65556
Orbit data source: Space-Track
GEESAT 5-07, 65556 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Mon, 08 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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65556 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: 16 hours ago
TLE from 16 hours ago
0 GEESAT 5-07
1 65556U 25201G 26171.32486869 .00001169 00000-0 16541-3 0 9997
2 65556 49.9900 24.5823 0013077 325.6273 34.3818 14.84151515 42266Epoch: 2026-06-20T07:47Z
TLE epoch observation values (Epoch: 2026-06-20T07:47:48.654Z)
Latitude
-0.00006°
Longitude
-0.9116°
Altitude
609.249 km
Speed
7.56 km/s
True Right ascension
01h 38m 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
10:19:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.158 km
Perigee altitude
607.863 km
Semi-major axis
6,995.147 km
Eccentricity
0.00131
Inclination
49.99°
RAAN
24.5823°
Arg. of periapsis
325.6273°
True anomaly
34.46654°
Mean anomaly
34.3818°
Eccentric anomaly
34.42416°
Mean motion
3.70978 °/min
Orbital period
97.04 mins
BSTAR
0.00016541
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Other satellites on launch #201 in the year 2025 (2025-09-08 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 5-07 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-21 00:29:21.703Z | 285.045° WNW | 2026-06-21 00:33:21.703Z | 214.105° SW | 27.919° | 2026-06-21 00:36:21.703Z | 165.835° S |
| 6 mins | 2026-06-21 16:17:21.703Z | 195.181° SSW | 2026-06-21 16:20:21.703Z | 127.942° SE | 31.465° | 2026-06-21 16:23:21.703Z | 74.319° E |
| 7 mins | 2026-06-21 17:58:21.703Z | 266.973° W | 2026-06-21 18:01:21.703Z | 332.165° NNW | 35.621° | 2026-06-21 18:05:21.703Z | 46.533° ENE |
| 5 mins | 2026-06-21 19:41:21.703Z | 315.395° NNW | 2026-06-21 19:43:21.703Z | 349.904° N | 21.427° | 2026-06-21 19:46:21.703Z | 40.035° NE |
| 6 mins | 2026-06-21 21:23:21.703Z | 326.405° NNW | 2026-06-21 21:26:21.703Z | 24.686° NE | 25.375° | 2026-06-21 21:29:21.703Z | 71.854° E |
| 7 mins | 2026-06-21 23:04:21.703Z | 304.896° NW | 2026-06-21 23:07:21.703Z | 312.257° NW | 43.68° | 2026-06-21 23:11:21.703Z | 124.092° SE |
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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