Showing default

ION-SCV-022, 66682

Orbit data source: Space-Track

ION-SCV-022, 66682 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Fri, 28 Nov 2025 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
66682, 2025-276S
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)
2025-11-28 (9 months 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, Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 ION-SCV-022
1 66682U 25276S   26238.19005010  .00000780  00000-0  70764-4 0  9990
2 66682  97.5231 306.3577 0004323 301.4885  58.5915 14.98009972 40555
Epoch: 2026-08-26T04:33Z
TLE epoch observation values (Epoch: 2026-08-26T04:33:40.328Z)
Latitude
-0.00004°
Longitude
-96.50694°
Altitude
574.537 km
Speed
7.574 km/s
True Right ascension
20h 25m 25s
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
09:53:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.05 km
Perigee altitude
567.042 km
Semi-major axis
6,948.183 km
Eccentricity
0.00043
Inclination
97.5231°
RAAN
306.3577°
Arg. of periapsis
301.4885°
True anomaly
58.63379°
Mean anomaly
58.5915°
Eccentric anomaly
58.61264°
Mean motion
3.74745 °/min
Orbital period
96.07 mins
BSTAR
0.000070764
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
|