DECAYED
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ICEYE-X16, 51008 (Decayed)

Orbit data source: Space-Track

ICEYE-X16, 51008 was a payload satellite owned by ICEYE (FI) in LEO that was launched on Thu, 13 Jan 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.

Not visible in the next 10 days
Identifier
51008, 2022-002AA
Orbit
Decayed
Last TLE update
10 months ago
Origin
Manufacturer
ICEYE
Mission
Decayed Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
2022-01-13 (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, 1.6 m
Radar Cross Section
1.837 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 10 months ago
0 ICEYE-X16
1 51008U 22002AA  24260.25594853  .15304442  25466-5  36584-3 0  9995
2 51008  97.3464 339.2457 0011843 267.6053  92.3894 16.45328635149178
Epoch: 2024-09-16T06:08Z
TLE epoch observation values (Epoch: 2024-09-16T06:08:33.952Z)
Latitude
-0.00001°
Longitude
-108.58334°
Altitude
155.257 km
Speed
7.813 km/s
True Right ascension
22h 36m 58s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
156.194 km
Perigee altitude
140.735 km
Semi-major axis
6,526.601 km
Eccentricity
0.00118
Inclination
97.3464°
RAAN
339.2457°
Arg. of periapsis
267.6053°
True anomaly
92.52498°
Mean anomaly
92.3894°
Eccentric anomaly
92.45719°
Mean motion
4.11635 °/min
Orbital period
87.46 mins
BSTAR
0.00036584
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