VSP RF A1, 59135
Orbit data source: Space-Track
VSP RF A1, 59135 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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59135 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: 9 hours ago
TLE from 9 hours ago
0 VSP RF A1
1 59135U 24043AP 25295.49908980 .00007086 00000-0 27560-3 0 9990
2 59135 97.5355 64.7225 0011137 4.2170 355.9160 15.26290776 90724Epoch: 2025-10-22T11:58Z
TLE epoch observation values (Epoch: 2025-10-22T11:58:41.358Z)
Latitude
-0.00004°
Longitude
-146.12164°
Altitude
482.379 km
Speed
7.628 km/s
True Right ascension
04h 18m 53s
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
15:58:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.517 km
Perigee altitude
476.233 km
Semi-major axis
6,862.012 km
Eccentricity
0.00111
Inclination
97.5355°
RAAN
64.7225°
Arg. of periapsis
4.217°
True anomaly
355.9069°
Mean anomaly
355.916°
Eccentric anomaly
355.91145°
Mean motion
3.81826 °/min
Orbital period
94.28 mins
BSTAR
0.0002756
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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 A1 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 | 2025-10-22 21:58:05.924Z | 358.414° N | 2025-10-22 22:01:05.924Z | 303.707° NW | 34.405° | 2025-10-22 22:04:05.924Z | 217.587° SW |
| 5 mins | 2025-10-23 08:35:05.924Z | 143.251° SSE | 2025-10-23 08:37:05.924Z | 39.318° NE | 38.627° | 2025-10-23 08:40:05.924Z | 355.961° N |
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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