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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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 A1
1 59135U 24043AP 26262.47581339 .00002074 00000-0 93603-4 0 9992
2 59135 97.5712 39.4545 0001172 102.7046 257.4321 15.22150525141342Epoch: 2026-09-19T11:25Z
TLE epoch observation values (Epoch: 2026-09-19T11:25:10.276Z)
Latitude
-0.00004°
Longitude
-130.22212°
Altitude
502.619 km
Speed
7.613 km/s
True Right ascension
02h 37m 49s
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
08:43:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.131 km
Perigee altitude
495.52 km
Semi-major axis
6,874.462 km
Eccentricity
0.00012
Inclination
97.5712°
RAAN
39.4545°
Arg. of periapsis
102.7046°
True anomaly
257.41899°
Mean anomaly
257.4321°
Eccentric anomaly
257.42555°
Mean motion
3.8079 °/min
Orbital period
94.54 mins
BSTAR
0.000093603
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-19 21:27:40.224Z | 43.975° NE | 2026-09-19 21:30:40.224Z | 109.852° ESE | 25.088° | 2026-09-19 21:32:40.224Z | 148.207° SSE |
| 5 mins | 2026-09-20 09:38:40.224Z | 196.649° SSW | 2026-09-20 09:40:40.224Z | 253.648° W | 44.731° | 2026-09-20 09:43:40.224Z | 331.104° NNW |
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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