GEESAT 5-02, 65551
Orbit data source: Space-Track
GEESAT 5-02, 65551 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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65551 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: 15 hours ago
TLE from 15 hours ago
0 GEESAT 5-02
1 65551U 25201B 26171.28751531 .00001187 00000-0 16751-3 0 9991
2 65551 49.9879 25.0339 0008130 338.7875 21.2726 14.84153176 42258Epoch: 2026-06-20T06:54Z
TLE epoch observation values (Epoch: 2026-06-20T06:54:01.322Z)
Latitude
0.00002°
Longitude
13.02411°
Altitude
611.49 km
Speed
7.558 km/s
True Right ascension
01h 40m 08s
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
08:41:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
622.693 km
Perigee altitude
611.319 km
Semi-major axis
6,995.143 km
Eccentricity
0.00081
Inclination
49.9879°
RAAN
25.0339°
Arg. of periapsis
338.7875°
True anomaly
21.30643°
Mean anomaly
21.2726°
Eccentric anomaly
21.28951°
Mean motion
3.70978 °/min
Orbital period
97.04 mins
BSTAR
0.00016751
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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 5-02 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-20 21:51:41.858Z | 318.911° NNW | 2026-06-20 21:54:41.858Z | 5.921° NNE | 25.987° | 2026-06-20 21:58:41.858Z | 75.638° E |
| 7 mins | 2026-06-20 23:33:41.858Z | 302.891° NW | 2026-06-20 23:36:41.858Z | 273.252° WNW | 44.675° | 2026-06-20 23:40:41.858Z | 127.767° SE |
| 7 mins | 2026-06-21 17:01:41.858Z | 229.67° WSW | 2026-06-21 17:04:41.858Z | 200.262° SSW | 43.883° | 2026-06-21 17:08:41.858Z | 57.966° ENE |
| 6 mins | 2026-06-21 18:44:41.858Z | 298.897° NW | 2026-06-21 18:46:41.858Z | 341.169° N | 26.771° | 2026-06-21 18:50:41.858Z | 44.807° NE |
| 6 mins | 2026-06-21 20:26:41.858Z | 322.349° NNW | 2026-06-21 20:28:41.858Z | 354.896° N | 20.862° | 2026-06-21 20:32:41.858Z | 56.302° ENE |
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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