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, Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 week ago

TLE from 1 week ago
0 ION SCV-008
1 55051U 23001AU  26155.27577081  .00007817  00000-0  28431-3 0  9992
2 55051  97.5704 251.3799 0016097  61.6750 298.6110 15.28414581189367
Epoch: 2026-06-04T06:37Z
TLE epoch observation values (Epoch: 2026-06-04T06:37:06.597Z)
Latitude
-0.00012°
Longitude
-100.61994°
Altitude
478.374 km
Speed
7.629 km/s
True Right ascension
16h 45m 31s
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
15:30:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.548 km
Perigee altitude
466.477 km
Semi-major axis
6,855.65 km
Eccentricity
0.00161
Inclination
97.5704°
RAAN
251.3799°
Arg. of periapsis
61.675°
True anomaly
298.44891°
Mean anomaly
298.611°
Eccentric anomaly
298.52997°
Mean motion
3.82358 °/min
Orbital period
94.15 mins
BSTAR
0.00028431
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|