VSP RF C1, 59136
Orbit data source: Space-Track
VSP RF C1, 59136 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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59136 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 C1
1 59136U 24043AQ 25289.59658853 .00007243 00000-0 26874-3 0 9998
2 59136 97.5305 59.0302 0010819 23.3931 336.7798 15.27852503 89855Epoch: 2025-10-16T14:19Z
TLE epoch observation values (Epoch: 2025-10-16T14:19:05.248Z)
Latitude
-0.00001°
Longitude
178.90429°
Altitude
478.509 km
Speed
7.63 km/s
True Right ascension
03h 56m 07s
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
21:16:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.613 km
Perigee altitude
471.775 km
Semi-major axis
6,857.331 km
Eccentricity
0.00108
Inclination
97.5305°
RAAN
59.0302°
Arg. of periapsis
23.3931°
True anomaly
336.73086°
Mean anomaly
336.7798°
Eccentric anomaly
336.75534°
Mean motion
3.82217 °/min
Orbital period
94.19 mins
BSTAR
0.00026874
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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 C1 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 09:18:54.567Z | 207.543° SW | 2025-10-17 09:20:54.567Z | 257.339° W | 27.75° | 2025-10-17 09:23:54.567Z | 324.841° NNW |
| 4 mins | 2025-10-17 22:19:54.567Z | 323.323° NNW | 2025-10-17 22:20:54.567Z | 298.757° NW | 22.774° | 2025-10-17 22:23:54.567Z | 235.527° WSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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