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, 1.0 m
Radar Cross Section
0.963 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 VSP RF C1
1 59136U 24043AQ 25346.68899439 .00008411 00000-0 30284-3 0 9997
2 59136 97.5355 116.7750 0010638 167.4522 192.6985 15.28788824 98574Epoch: 2025-12-12T16:32Z
TLE epoch observation values (Epoch: 2025-12-12T16:32:09.115Z)
Latitude
0.00005°
Longitude
147.11°
Altitude
489.649 km
Speed
7.616 km/s
True Right ascension
07h 47m 05s
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
00:47:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.683 km
Perigee altitude
469.1 km
Semi-major axis
6,854.529 km
Eccentricity
0.00106
Inclination
97.5355°
RAAN
116.775°
Arg. of periapsis
167.4522°
True anomaly
192.67174°
Mean anomaly
192.6985°
Eccentric anomaly
192.68512°
Mean motion
3.82452 °/min
Orbital period
94.13 mins
BSTAR
0.00030284
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-14 07:58:03.945Z | 101.5° ESE | 2025-12-14 08:00:03.945Z | 63.153° ENE | 15.906° | 2025-12-14 08:02:03.945Z | 28.359° NE |
| 4 mins | 2025-12-14 09:31:03.945Z | 217.29° SW | 2025-12-14 09:33:03.945Z | 267.409° W | 24.468° | 2025-12-14 09:35:03.945Z | 313.027° NW |
| 4 mins | 2025-12-14 22:31:03.945Z | 324.779° NNW | 2025-12-14 22:33:03.945Z | 278.017° WNW | 19.443° | 2025-12-14 22:35:03.945Z | 241.81° WSW |
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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