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ICEYE-X12, 48914

Orbit data source: Space-Track

ICEYE-X12, 48914 is a payload satellite owned by ICEYE (FI) in SSO 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

ICEYE-X12 details

Identifier	48914, 2021-059AM
Orbit	SSO
Last TLE update	10 hours ago
Origin	ICEYE (FI / FIN)
Manufacturer	ICEYE
Mission	Operational Commercial Radar Imaging
Bus & Motor	ICEYE, Unknown motor
Mass	80 kg wet, 80 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 + 1 Pan, 3.25 m
Radar Cross Section	1.837 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 10 hours ago

0 ICEYE-X12
1 48914U 21059AM  25014.88993876  .01839223  27314-2  21284-2 0  9999
2 48914  97.6223 173.9935 0008076 314.0442  46.0174 16.09538668197464

Epoch: 2025-01-14T21:21Z

Definitive object data (Epoch: 2025-01-14T21:21:30.708Z)

Latitude	-0.00011°
Longitude	99.02542°
Altitude	247.598 km
Speed	7.76 km/s
True Right ascension	11h 35m 58s
True Declination	0° 00' 00"
Sunlit	Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude	-67.72429°
Longitude	-99.44984°
Altitude	266.159 km
Speed	7.747 km/s
Apparent Right ascension	20h 47m 30s
Apparent Declination	-55° 07' 33"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	07:59:46
Azimuth	203.623° SW
Elevation	-72.843°
Doppler factor	1

Orbital elements

Apogee altitude	250.315 km
Perigee altitude	239.618 km
Semi-major axis	6,623.103 km
Eccentricity	0.0008076
Inclination	97.6223°
RAAN	173.9935°
Arg. of periapsis	314.0442°
True anomaly	46.08404°
Mean anomaly	46.0174°
Eccentric anomaly	46.05071°
Mean motion	4.02671 °/min
BSTAR	0.0021284
Orbital period	89.4 mins