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: 4 hours ago
TLE from 4 hours ago
0 VSP RF B1
1 59137U 24043AR 26285.33705425 .00004084 00000-0 17760-3 0 9990
2 59137 97.5789 63.4196 0001247 112.9919 247.1448 15.22844591144861Epoch: 2026-10-12T08:05Z
TLE epoch observation values (Epoch: 2026-10-12T08:05:21.487Z)
Latitude
-0.00009°
Longitude
-78.83685°
Altitude
500.688 km
Speed
7.614 km/s
True Right ascension
04h 13m 40s
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
06:25:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.092 km
Perigee altitude
493.378 km
Semi-major axis
6,872.372 km
Eccentricity
0.00012
Inclination
97.5789°
RAAN
63.4196°
Arg. of periapsis
112.9919°
True anomaly
247.13163°
Mean anomaly
247.1448°
Eccentric anomaly
247.13822°
Mean motion
3.80963 °/min
Orbital period
94.5 mins
BSTAR
0.0001776
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-12 21:17:06.443Z | 53.787° ENE | 2026-10-12 21:19:06.443Z | 87.343° E | 16.266° | 2026-10-12 21:21:06.443Z | 125.048° SE |
| 5 mins | 2026-10-12 22:51:06.443Z | 336.836° NNW | 2026-10-12 22:53:06.443Z | 289.258° WNW | 28.464° | 2026-10-12 22:56:06.443Z | 229.895° WSW |
| 5 mins | 2026-10-13 09:28:06.443Z | 175.521° S | 2026-10-13 09:30:06.443Z | 313.719° NW | 69.595° | 2026-10-13 09:33:06.443Z | 344.759° N |
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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