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, 1.5 m
Radar Cross Section
0.969 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 VSP RF B1
1 59137U 24043AR 25289.61496818 .00006840 00000-0 26166-3 0 9999
2 59137 97.5309 58.8710 0011137 23.0093 337.1642 15.26857485 89845Epoch: 2025-10-16T14:45Z
TLE epoch observation values (Epoch: 2025-10-16T14:45:33.250Z)
Latitude
-0.00006°
Longitude
172.11031°
Altitude
481.265 km
Speed
7.629 km/s
True Right ascension
03h 55m 29s
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
21:16:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.816 km
Perigee altitude
474.535 km
Semi-major axis
6,860.313 km
Eccentricity
0.00111
Inclination
97.5309°
RAAN
58.871°
Arg. of periapsis
23.0093°
True anomaly
337.11461°
Mean anomaly
337.1642°
Eccentric anomaly
337.13941°
Mean motion
3.81968 °/min
Orbital period
94.25 mins
BSTAR
0.00026166
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-17 08:11:53.194Z | 130.28° SE | 2025-10-17 08:14:53.194Z | 62.677° ENE | 25.877° | 2025-10-17 08:16:53.194Z | 18.255° NNE |
| 4 mins | 2025-10-17 21:13:53.194Z | 47.638° ENE | 2025-10-17 21:14:53.194Z | 76.71° E | 31.38° | 2025-10-17 21:17:53.194Z | 163.523° S |
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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