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
0.963 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 VSP RF B1
1 59137U 24043AR 26035.31523432 .00000402 00000-0 17720-4 0 9994
2 59137 97.5393 170.7522 0009880 353.1594 6.9508 15.27584560106741Epoch: 2026-02-04T07:33Z
TLE epoch observation values (Epoch: 2026-02-04T07:33:56.245Z)
Latitude
-0.00005°
Longitude
-77.21573°
Altitude
479.402 km
Speed
7.63 km/s
True Right ascension
11h 23m 00s
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
19:16:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.773 km
Perigee altitude
473.221 km
Semi-major axis
6,858.134 km
Eccentricity
0.00099
Inclination
97.5393°
RAAN
170.7522°
Arg. of periapsis
353.1594°
True anomaly
6.96452°
Mean anomaly
6.9508°
Eccentric anomaly
6.95766°
Mean motion
3.8215 °/min
Orbital period
94.2 mins
BSTAR
0.00001772
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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 | 2026-02-09 21:45:09.958Z | 14.417° NNE | 2026-02-09 21:48:09.958Z | 60.172° ENE | 44.452° | 2026-02-09 21:51:09.958Z | 189.493° SSW |
| 4 mins | 2026-02-10 08:21:09.958Z | 116.74° SE | 2026-02-10 08:23:09.958Z | 66.8° ENE | 24.357° | 2026-02-10 08:25:09.958Z | 21.731° 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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