VRSS-2, 42954
Orbit data source: Space-Track
VRSS-2, 42954 is a payload satellite owned by ABAE (VE) in SSO that was launched on Mon, 09 Oct 2017 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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42954 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
942 kg wet, ~900 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 4.0 m
Radar Cross Section
8.358 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 VRSS-2
1 42954U 17060A 25308.87182554 .00001133 00000-0 15357-3 0 9998
2 42954 97.6841 351.3804 0018636 111.7469 248.5730 14.80660180435250Epoch: 2025-11-04T20:55Z
TLE epoch observation values (Epoch: 2025-11-04T20:55:25.726Z)
Latitude
-0°
Longitude
-6.82942°
Altitude
635.061 km
Speed
7.538 km/s
True Right ascension
23h 25m 31s
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
21:44:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
637.321 km
Perigee altitude
611.222 km
Semi-major axis
7,002.408 km
Eccentricity
0.00186
Inclination
97.6841°
RAAN
351.3804°
Arg. of periapsis
111.7469°
True anomaly
248.37438°
Mean anomaly
248.573°
Eccentric anomaly
248.47367°
Mean motion
3.70401 °/min
Orbital period
97.19 mins
BSTAR
0.00015357
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Other satellites on launch #60 in the year 2017 (2017-10-09 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-2 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 | 2025-11-05 01:57:06.081Z | 101.52° ESE | 2025-11-05 01:59:06.081Z | 69.668° E | 17.59° | 2025-11-05 02:02:06.081Z | 24.213° NE |
| 6 mins | 2025-11-05 03:33:06.081Z | 209.332° SW | 2025-11-05 03:35:06.081Z | 256.926° W | 31.341° | 2025-11-05 03:39:06.081Z | 329.953° NNW |
| 6 mins | 2025-11-05 15:21:06.081Z | 37.353° NE | 2025-11-05 15:24:06.081Z | 109.135° ESE | 32.057° | 2025-11-05 15:27:06.081Z | 163.727° S |
| 4 mins | 2025-11-05 16:58:06.081Z | 321.179° NNW | 2025-11-05 17:00:06.081Z | 287.672° WNW | 16.599° | 2025-11-05 17:02:06.081Z | 257.46° W |
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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