VSP RF B1, 59137
Orbit data source: Space-Track
VSP RF B1, 59137 is a payload satellite owned by Aerospacelab (BE) in SSO that was launched on Mon, 04 Mar 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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59137 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
BE / BELRelated business
Manufacturer
Aerospacelab
Mission
Operational Commercial Sigint
Bus & Motor
AEROSP, Unknown motor
Mass
~200 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.969 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 VSP RF B1
1 59137U 24043AR 25336.33077000 .00007212 00000-0 26984-3 0 9991
2 59137 97.5357 106.0420 0010086 204.3730 155.7033 15.27581752 96978Epoch: 2025-12-02T07:56Z
TLE epoch observation values (Epoch: 2025-12-02T07:56:18.527Z)
Latitude
-0.00008°
Longitude
-84.45265°
Altitude
492.451 km
Speed
7.615 km/s
True Right ascension
07h 04m 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
11:09:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.922 km
Perigee altitude
473.088 km
Semi-major axis
6,858.142 km
Eccentricity
0.00101
Inclination
97.5357°
RAAN
106.042°
Arg. of periapsis
204.373°
True anomaly
155.7508°
Mean anomaly
155.7033°
Eccentric anomaly
155.72706°
Mean motion
3.8215 °/min
Orbital period
94.2 mins
BSTAR
0.00026984
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Other satellites on launch #43 in the year 2024 (2024-03-04 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.VSP RF B1 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-02 21:04:48.462Z | 36.883° NE | 2025-12-02 21:07:48.462Z | 95.92° ESE | 24.681° | 2025-12-02 21:10:48.462Z | 156.339° SSE |
| 5 mins | 2025-12-03 09:13:48.462Z | 198.245° SSW | 2025-12-03 09:15:48.462Z | 256.958° W | 34.307° | 2025-12-03 09:18:48.462Z | 331.019° 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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