Showing default

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.

Loading next visibility...
Identifier
59135, 2024-043AP
Orbit
SSO
Country
Flag of BEBE / BEL
Related business
Manufacturer
Aerospacelab
Mission
Operational Commercial Sigint
Bus & Motor
AEROSP, Unknown motor
Mass
~200 kg wet, ~200 kg dry
Launch date (UTC)
2024-03-04 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 VSP RF A1
1 59135U 24043AP  26079.79861516  .00000410  00000-0  18662-4 0  9995
2 59135  97.5271 215.4050 0010458 182.7946 177.3235 15.26329518113508
Epoch: 2026-03-20T19:10Z
TLE epoch observation values (Epoch: 2026-03-20T19:10:00.349Z)
Latitude
-0.0001°
Longitude
109.57505°
Altitude
497.065 km
Speed
7.612 km/s
True Right ascension
14h 21m 37s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
20:38:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.935 km
Perigee altitude
476.583 km
Semi-major axis
6,861.896 km
Eccentricity
0.00105
Inclination
97.5271°
RAAN
215.405°
Arg. of periapsis
182.7946°
True anomaly
177.32909°
Mean anomaly
177.3235°
Eccentric anomaly
177.3263°
Mean motion
3.81836 °/min
Orbital period
94.28 mins
BSTAR
0.000018662
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|