ION SCV-003, 48912 (Decayed)

Orbit data source: Space-Track

ION SCV-003, 48912 was a payload satellite owned by D-ORBIT (IT) in LEO that was launched on Wed, 30 Jun 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets 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.

Not visible in the next 10 days

ION SCV-003 details

Identifier	48912, 2021-059AK
Orbit	Decayed
Last TLE update	1 month ago
Origin	D-ORBIT (IT)
Manufacturer	D-ORBIT
Mission	Decayed Commercial Technology
Bus & Motor	ION-SC, PM200
Mass	220 kg wet, 150 kg dry
Launch date (UTC)	2021-06-30 (4 years ago)
Launch vehicle	FALCON 9
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Box, 0.4 m
Radar Cross Section	0.240 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 month ago

0 ION SCV-003
1 48912U 21059AK  24343.90367833  .30299551  29007-5  15470-3 0  9993
2 48912  97.5956 147.2839 0008524 244.8326 251.9010 16.55712356192718

Epoch: 2024-12-08T21:41Z

Definitive object data (Epoch: 2024-12-08T21:41:17.807Z)

Latitude	42.98728°
Longitude	-69.07643°
Altitude	132.583 km
Speed	7.83 km/s
True Right ascension	22h 17m 31s
True Declination	42° 47' 57"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	126.672 km
Perigee altitude	115.593 km
Semi-major axis	6,499.27 km
Eccentricity	0.0008524
Inclination	97.5956°
RAAN	147.2839°
Arg. of periapsis	244.8326°
True anomaly	251.80819°
Mean anomaly	251.901°
Eccentric anomaly	251.85459°
Mean motion	4.14235 °/min
BSTAR	0.0001547
Orbital period	86.91 mins