VRSS-1, 38782
Orbit data source: Space-Track
VRSS-1, 38782 is a payload satellite owned by ABAE (VE) in SSO that was launched on Sat, 29 Sep 2012 UTC via a CHANG ZHENG 2D launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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38782 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / VENZRelated business
Manufacturer
DFH
Mission
Operational Civil Imaging
Bus & Motor
CAST-2000, AOCS
Mass
880 kg wet, ~880 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.0 m
Radar Cross Section
4.991 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 VRSS-1
1 38782U 12052A 25310.94897495 .00001753 00000-0 24116-3 0 9997
2 38782 97.5927 294.0958 0016450 241.1289 118.8273 14.79385882706748Epoch: 2025-11-06T22:46Z
TLE epoch observation values (Epoch: 2025-11-06T22:46:31.435Z)
Latitude
-0.00005°
Longitude
-93.93513°
Altitude
639.868 km
Speed
7.535 km/s
True Right ascension
19h 36m 22s
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
04:05:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
639.817 km
Perigee altitude
616.766 km
Semi-major axis
7,006.428 km
Eccentricity
0.00165
Inclination
97.5927°
RAAN
294.0958°
Arg. of periapsis
241.1289°
True anomaly
118.99228°
Mean anomaly
118.8273°
Eccentric anomaly
118.90981°
Mean motion
3.70082 °/min
Orbital period
97.28 mins
BSTAR
0.00024116
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Other satellites on launch #52 in the year 2012 (2012-09-29 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.VRSS-1 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-07 10:44:06.065Z | 56.133° ENE | 2025-11-07 10:47:06.065Z | 99.514° ESE | 14.51° | 2025-11-07 10:49:06.065Z | 127.061° SE |
| 7 mins | 2025-11-07 12:20:06.065Z | 353.613° N | 2025-11-07 12:23:06.065Z | 291.116° WNW | 35.237° | 2025-11-07 12:27:06.065Z | 216.001° SW |
| 7 mins | 2025-11-07 23:15:06.065Z | 180.178° SSW | 2025-11-07 23:18:06.065Z | 245.533° WSW | 42.059° | 2025-11-07 23:22:06.065Z | 340.459° N |
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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