Showing default

VSP ROSE, 59124

Orbit data source: Space-Track

VSP ROSE, 59124 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
59124, 2024-043AC
Orbit
SSO
Country
Flag of BEBE / BEL
Related business
Manufacturer
Aerospacelab
Mission
Operational Commercial Imaging
Bus & Motor
AEROSP, Unknown motor
Mass
~200 kg wet, ~200 kg dry
Launch date (UTC)
2024-03-04 (3 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, Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 VSP ROSE
1 59124U 24043AC  26304.20304291  .00000006  00000-0  29640-5 0  9992
2 59124  97.5811  83.0000 0012682 117.5090 242.7440 15.29364855147774
Epoch: 2026-10-31T04:52Z
TLE epoch observation values (Epoch: 2026-10-31T04:52:22.907Z)
Latitude
-0.00004°
Longitude
-29.60758°
Altitude
484.799 km
Speed
7.621 km/s
True Right ascension
05h 32m 00s
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
07:44:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.361 km
Perigee altitude
465.98 km
Semi-major axis
6,852.808 km
Eccentricity
0.00127
Inclination
97.5811°
RAAN
83°
Arg. of periapsis
117.509°
True anomaly
242.6149°
Mean anomaly
242.744°
Eccentric anomaly
242.67944°
Mean motion
3.82596 °/min
Orbital period
94.09 mins
BSTAR
0.000002964
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
|