Showing default

ION SCV-002, 47504

Orbit data source: Space-Track

ION SCV-002, 47504 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Sun, 24 Jan 2021 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
47504, 2021-006CV
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)
2021-01-24 (5 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-002
1 47504U 21006CV  26082.43443449  .00015522  00000-0  36644-3 0  9993
2 47504  97.1153  86.3419 0013838  73.1751 287.1013 15.41848505286803
Epoch: 2026-03-23T10:25Z
TLE epoch observation values (Epoch: 2026-03-23T10:25:35.139Z)
Latitude
-0.00009°
Longitude
109.019°
Altitude
441.019 km
Speed
7.649 km/s
True Right ascension
05h 45m 22s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
00:11:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.01 km
Perigee altitude
428.147 km
Semi-major axis
6,815.715 km
Eccentricity
0.00138
Inclination
97.1153°
RAAN
86.3419°
Arg. of periapsis
73.1751°
True anomaly
286.94966°
Mean anomaly
287.1013°
Eccentric anomaly
287.02549°
Mean motion
3.85723 °/min
Orbital period
93.33 mins
BSTAR
0.00036644
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|