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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Identifier
Orbit
Country
VE / 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: 22 hours ago
TLE from 22 hours ago
0 VRSS-2
1 42954U 17060A 26172.51058861 .00000525 00000-0 73605-4 0 9997
2 42954 97.6507 210.0432 0018651 85.8924 274.4420 14.81199529469099Epoch: 2026-06-21T12:15Z
TLE epoch observation values (Epoch: 2026-06-21T12:15:14.855Z)
Latitude
-0.00011°
Longitude
116.5215°
Altitude
627.583 km
Speed
7.545 km/s
True Right ascension
14h 00m 10s
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
21:38:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
635.626 km
Perigee altitude
609.512 km
Semi-major axis
7,000.706 km
Eccentricity
0.00187
Inclination
97.6507°
RAAN
210.0432°
Arg. of periapsis
85.8924°
True anomaly
274.22888°
Mean anomaly
274.442°
Eccentric anomaly
274.33544°
Mean motion
3.70536 °/min
Orbital period
97.16 mins
BSTAR
0.000073605
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 14:45:52.667Z | 32.987° NE | 2026-06-22 14:49:52.667Z | 104.214° ESE | 28.272° | 2026-06-22 14:52:52.667Z | 157.099° SSE |
| 4 mins | 2026-06-22 16:23:52.667Z | 324.349° NNW | 2026-06-22 16:25:52.667Z | 288.103° WNW | 19.387° | 2026-06-22 16:27:52.667Z | 254.643° W |
| 5 mins | 2026-06-23 01:41:52.667Z | 112.057° ESE | 2026-06-23 01:43:52.667Z | 77.604° E | 21.846° | 2026-06-23 01:46:52.667Z | 23.054° NE |
| 6 mins | 2026-06-23 03:17:52.667Z | 215.531° SW | 2026-06-23 03:20:52.667Z | 276.204° WNW | 24.37° | 2026-06-23 03:23:52.667Z | 322.053° NNW |
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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