GEESAT 5-03, 65552
Orbit data source: Space-Track
GEESAT 5-03, 65552 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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65552 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: 23 hours ago
TLE from 23 hours ago
0 GEESAT 5-03
1 65552U 25201C 26171.01082462 .00001187 00000-0 16744-3 0 9995
2 65552 49.9884 26.2574 0010754 273.6506 86.3203 14.84190972 42215Epoch: 2026-06-20T00:15Z
TLE epoch observation values (Epoch: 2026-06-20T00:15:35.247Z)
Latitude
0.00003°
Longitude
114.12898°
Altitude
616.195 km
Speed
7.552 km/s
True Right ascension
01h 45m 01s
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
10:18:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
624.409 km
Perigee altitude
609.364 km
Semi-major axis
6,995.024 km
Eccentricity
0.00108
Inclination
49.9884°
RAAN
26.2574°
Arg. of periapsis
273.6506°
True anomaly
86.44329°
Mean anomaly
86.3203°
Eccentric anomaly
86.38179°
Mean motion
3.70988 °/min
Orbital period
97.04 mins
BSTAR
0.00016744
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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 5-03 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 23:22:25.845Z | 306.505° NW | 2026-06-20 23:25:25.845Z | 331.839° NNW | 43.715° | 2026-06-20 23:29:25.845Z | 120.976° SE |
| 4 mins | 2026-06-21 01:05:25.845Z | 250.75° W | 2026-06-21 01:06:25.845Z | 234.433° WSW | 17.292° | 2026-06-21 01:09:25.845Z | 189.935° SSW |
| 6 mins | 2026-06-21 16:51:25.845Z | 219.072° SW | 2026-06-21 16:53:25.845Z | 183.125° SSW | 41.447° | 2026-06-21 16:57:25.845Z | 61.729° ENE |
| 6 mins | 2026-06-21 18:33:25.845Z | 293.381° NW | 2026-06-21 18:35:25.845Z | 336.974° NNW | 28.699° | 2026-06-21 18:39:25.845Z | 44.211° NE |
| 6 mins | 2026-06-21 20:15:25.845Z | 319.92° NNW | 2026-06-21 20:17:25.845Z | 351.971° N | 20.781° | 2026-06-21 20:21:25.845Z | 53.419° ENE |
| 6 mins | 2026-06-21 21:57:25.845Z | 323.97° NNW | 2026-06-21 22:00:25.845Z | 29.795° NE | 31.047° | 2026-06-21 22:03:25.845Z | 84.31° E |
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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