Showing default

ION SCV-008, 55051

Orbit data source: Space-Track

ION SCV-008, 55051 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Tue, 03 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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
55051, 2023-001AU
Orbit
SSO
Country
Flag of ITIT
Related business
Manufacturer
D-ORBIT
Mission
Operational Commercial Technology
Bus & Motor
ION-SC, PM200
Mass
220 kg wet, 150 kg dry
Launch date (UTC)
2023-01-03 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.240 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 ION SCV-008
1 55051U 23001AU  25345.25963980  .00011601  00000-0  45772-3 0  9990
2 55051  97.5772  73.8310 0014904 318.4114  41.5989 15.25612785162655
Epoch: 2025-12-11T06:13Z
TLE epoch observation values (Epoch: 2025-12-11T06:13:52.878Z)
Latitude
-0.00004°
Longitude
-99.8575°
Altitude
484.39 km
Speed
7.627 km/s
True Right ascension
04h 55m 19s
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
13:09:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.142 km
Perigee altitude
475.682 km
Semi-major axis
6,864.049 km
Eccentricity
0.00149
Inclination
97.5772°
RAAN
73.831°
Arg. of periapsis
318.4114°
True anomaly
41.71245°
Mean anomaly
41.5989°
Eccentric anomaly
41.65566°
Mean motion
3.81656 °/min
Orbital period
94.33 mins
BSTAR
0.00045772
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
|