Showing default

ION SCV-013, 58300

Orbit data source: Space-Track

ION SCV-013, 58300 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Sat, 11 Nov 2023 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
58300, 2023-174AW
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)
2023-11-11 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
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: 8 hours ago

TLE from 8 hours ago
0 ION SCV-013
1 58300U 23174AW  26080.99489571  .00002979  00000-0  19334-3 0  9991
2 58300  97.6252 137.2076 0100812 131.8834 229.1048 15.04695224128426
Epoch: 2026-03-21T23:52Z
TLE epoch observation values (Epoch: 2026-03-21T23:52:38.989Z)
Latitude
-0.00004°
Longitude
-40.46247°
Altitude
601.655 km
Speed
7.534 km/s
True Right ascension
09h 08m 49s
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
12:39:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
619.275 km
Perigee altitude
479.598 km
Semi-major axis
6,927.574 km
Eccentricity
0.01008
Inclination
97.6252°
RAAN
137.2076°
Arg. of periapsis
131.8834°
True anomaly
228.23874°
Mean anomaly
229.1048°
Eccentric anomaly
228.67105°
Mean motion
3.76419 °/min
Orbital period
95.64 mins
BSTAR
0.00019334
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|