Showing default

ION SCV-012, 60573

Orbit data source: Space-Track

ION SCV-012, 60573 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Fri, 16 Aug 2024 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
60573, 2024-149DK
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)
2024-08-16 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 2.0 m
Radar Cross Section
0.240 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 ION SCV-012
1 60573U 24149DK  26310.72688973  .00000696  00000-0  68492-4 0  9997
2 60573  97.6647  21.6563 0002719 351.7159   8.4016 14.95172074121211
Epoch: 2026-11-06T17:26Z
TLE epoch observation values (Epoch: 2026-11-06T17:26:43.272Z)
Latitude
-0.00009°
Longitude
74.03366°
Altitude
583.015 km
Speed
7.57 km/s
True Right ascension
01h 26m 37s
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
22:59:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.74 km
Perigee altitude
576.957 km
Semi-major axis
6,956.986 km
Eccentricity
0.00027
Inclination
97.6647°
RAAN
21.6563°
Arg. of periapsis
351.7159°
True anomaly
8.40615°
Mean anomaly
8.4016°
Eccentric anomaly
8.40388°
Mean motion
3.74034 °/min
Orbital period
96.25 mins
BSTAR
0.000068492
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
|