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: 14 hours ago
TLE from 14 hours ago
0 VSP RF A1
1 59135U 24043AP 26308.55499253 .00002164 00000-0 96862-4 0 9995
2 59135 97.5774 85.8758 0001988 90.0941 270.0523 15.22381596148356Epoch: 2026-11-04T13:19Z
TLE epoch observation values (Epoch: 2026-11-04T13:19:11.354Z)
Latitude
-0°
Longitude
-157.72314°
Altitude
501.747 km
Speed
7.613 km/s
True Right ascension
05h 43m 30s
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
23:27:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.996 km
Perigee altitude
494.263 km
Semi-major axis
6,873.766 km
Eccentricity
0.0002
Inclination
97.5774°
RAAN
85.8758°
Arg. of periapsis
90.0941°
True anomaly
270.02952°
Mean anomaly
270.0523°
Eccentric anomaly
270.04091°
Mean motion
3.80847 °/min
Orbital period
94.53 mins
BSTAR
0.000096862
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-05 08:24:14.865Z | 105.912° ESE | 2026-11-05 08:26:14.865Z | 70.767° E | 16.954° | 2026-11-05 08:28:14.865Z | 33.716° NE |
| 4 mins | 2026-11-05 09:58:14.865Z | 221.06° SW | 2026-11-05 10:00:14.865Z | 275.252° WNW | 27.9° | 2026-11-05 10:02:14.865Z | 316.477° NNW |
| 4 mins | 2026-11-05 23:01:14.865Z | 324.314° NNW | 2026-11-05 23:03:14.865Z | 280.063° WNW | 20.685° | 2026-11-05 23:05:14.865Z | 244.436° 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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