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 (6 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: 20 hours ago

TLE from 20 hours ago
0 ION SCV-002
1 47504U 21006CV  26207.43152227  .00013559  00000-0  28963-3 0  9996
2 47504  97.1134 208.5229 0009608 346.1212  13.9772 15.44916501306089
Epoch: 2026-07-26T10:21Z
TLE epoch observation values (Epoch: 2026-07-26T10:21:23.524Z)
Latitude
0.00001°
Longitude
109.04534°
Altitude
428.406 km
Speed
7.658 km/s
True Right ascension
13h 54m 05s
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
19:51:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
435.084 km
Perigee altitude
422.004 km
Semi-major axis
6,806.681 km
Eccentricity
0.00096
Inclination
97.1134°
RAAN
208.5229°
Arg. of periapsis
346.1212°
True anomaly
14.00382°
Mean anomaly
13.9772°
Eccentric anomaly
13.99051°
Mean motion
3.86492 °/min
Orbital period
93.15 mins
BSTAR
0.00028963
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
|