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: 8 hours ago
TLE from 8 hours ago
0 VRSS-2
1 42954U 17060A 25261.29379594 .00000862 00000-0 11895-3 0 9995
2 42954 97.6924 305.7854 0015743 268.4284 91.5125 14.80498156428215Epoch: 2025-09-18T07:03Z
TLE epoch observation values (Epoch: 2025-09-18T07:03:03.969Z)
Latitude
-0.00005°
Longitude
-157.43859°
Altitude
631.089 km
Speed
7.543 km/s
True Right ascension
20h 23m 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
07:31:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
635.808 km
Perigee altitude
613.758 km
Semi-major axis
7,002.92 km
Eccentricity
0.00157
Inclination
97.6924°
RAAN
305.7854°
Arg. of periapsis
268.4284°
True anomaly
91.69283°
Mean anomaly
91.5125°
Eccentric anomaly
91.60267°
Mean motion
3.7036 °/min
Orbital period
97.2 mins
BSTAR
0.00011895
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-18 15:43:27.727Z | 18.478° NNE | 2025-09-18 15:47:27.727Z | 86.139° E | 42.276° | 2025-09-18 15:51:27.727Z | 182.739° SSW |
| 6 mins | 2025-09-19 02:39:27.727Z | 137.58° SSE | 2025-09-19 02:42:27.727Z | 61.018° ENE | 35.489° | 2025-09-19 02:45:27.727Z | 4.637° NNE |
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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