VENUS, 42901
Orbit data source: Space-Track
VENUS, 42901 is an Israeli payload satellite in SSO that was launched on Wed, 02 Aug 2017 UTC via a VEGA launch vehicle from the French Guiana (FRGUI). 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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42901 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ISRARelated business
Manufacturer
IAI
Mission
Non-operational Civil Imaging
Bus & Motor
VENMS, HET-300
Mass
264 kg wet, ~250 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.3 m
Radar Cross Section
3.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 VENUS
1 42901U 17044B 25308.59446497 .00007426 00000-0 44376-3 0 9994
2 42901 97.3043 350.1040 0005100 70.8319 289.3464 15.11349393446998Epoch: 2025-11-04T14:16Z
TLE epoch observation values (Epoch: 2025-11-04T14:16:01.773Z)
Latitude
0.00005°
Longitude
92.01736°
Altitude
533.999 km
Speed
7.596 km/s
True Right ascension
23h 20m 24s
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
19:18:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
532.58 km
Perigee altitude
525.534 km
Semi-major axis
6,907.194 km
Eccentricity
0.00051
Inclination
97.3043°
RAAN
350.104°
Arg. of periapsis
70.8319°
True anomaly
289.29125°
Mean anomaly
289.3464°
Eccentric anomaly
289.31882°
Mean motion
3.78086 °/min
Orbital period
95.22 mins
BSTAR
0.00044376
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Other satellites on launch #44 in the year 2017 (2017-08-02 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.VENUS 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 | 2025-11-05 03:05:50.762Z | 176.17° S | 2025-11-05 03:08:50.762Z | 215.699° SW | 41.097° | 2025-11-05 03:12:50.762Z | 342.419° N |
| 5 mins | 2025-11-05 16:15:50.762Z | 343.633° N | 2025-11-05 16:17:50.762Z | 293.807° NW | 31.118° | 2025-11-05 16:20:50.762Z | 223.853° SW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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