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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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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 VSP RF B1
1 59137U 24043AR 26286.91405294 .00003573 00000-0 15571-3 0 9996
2 59137 97.5791 65.0107 0001276 113.9288 246.2082 15.22855155145106Epoch: 2026-10-13T21:56Z
TLE epoch observation values (Epoch: 2026-10-13T21:56:14.174Z)
Latitude
0.00001°
Longitude
73.48035°
Altitude
500.677 km
Speed
7.614 km/s
True Right ascension
04h 20m 02s
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
01:47:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.08 km
Perigee altitude
493.326 km
Semi-major axis
6,872.34 km
Eccentricity
0.00013
Inclination
97.5791°
RAAN
65.0107°
Arg. of periapsis
113.9288°
True anomaly
246.19482°
Mean anomaly
246.2082°
Eccentric anomaly
246.20151°
Mean motion
3.80966 °/min
Orbital period
94.5 mins
BSTAR
0.00015571
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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 | 2026-10-14 09:06:37.576Z | 148.329° SSE | 2026-10-14 09:09:37.576Z | 52.942° ENE | 51.703° | 2026-10-14 09:12:37.576Z | 358.374° N |
| 6 mins | 2026-10-14 22:09:37.576Z | 15.758° NNE | 2026-10-14 22:12:37.576Z | 164.442° S | 69.145° | 2026-10-14 22:15:37.576Z | 189.375° SSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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