Showing default

ION SCV-015, 58469

Orbit data source: Space-Track

ION SCV-015, 58469 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Fri, 01 Dec 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
58469, 2023-185H
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)
2023-12-01 (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: 5 hours ago

TLE from 5 hours ago
0 ION SCV-015
1 58469U 23185H   26092.32803513  .00010580  00000-0  34413-3 0  9997
2 58469  97.5760 179.2721 0009513  17.8313 342.3260 15.32032324129465
Epoch: 2026-04-02T07:52Z
TLE epoch observation values (Epoch: 2026-04-02T07:52:22.235Z)
Latitude
-0.00002°
Longitude
-129.49864°
Altitude
466.643 km
Speed
7.636 km/s
True Right ascension
11h 57m 05s
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
18:30:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.218 km
Perigee altitude
460.195 km
Semi-major axis
6,844.844 km
Eccentricity
0.00095
Inclination
97.576°
RAAN
179.2721°
Arg. of periapsis
17.8313°
True anomaly
342.29287°
Mean anomaly
342.326°
Eccentric anomaly
342.30944°
Mean motion
3.83264 °/min
Orbital period
93.93 mins
BSTAR
0.00034413
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
|