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ICEYE-X8, 47510

Orbit data source: Space-Track

ICEYE-X8, 47510 is a payload satellite owned by ICEYE (FI) in LEO that was launched on Sun, 24 Jan 2021 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
47510, 2021-006DB
Orbit
LEO
Country
Flag of FIFI / FIN
Related business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
2021-01-24 (5 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
Last TLE update: 3 weeks ago

TLE from 3 weeks ago
0 ICEYE-X8
1 47510U 21006DB  25318.42152150  .13776352  24193-5  55836-3 0  9993
2 47510  97.2200  29.2528 0010203 285.6686  74.3489 16.42888174268374
Epoch: 2025-11-14T10:06Z
TLE epoch observation values (Epoch: 2025-11-14T10:06:59.457Z)
Latitude
-0.00008°
Longitude
-176.26018°
Altitude
159.598 km
Speed
7.811 km/s
True Right ascension
01h 57m 00s
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
01:19:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
161.592 km
Perigee altitude
148.261 km
Semi-major axis
6,533.064 km
Eccentricity
0.00102
Inclination
97.22°
RAAN
29.2528°
Arg. of periapsis
285.6686°
True anomaly
74.46152°
Mean anomaly
74.3489°
Eccentric anomaly
74.40521°
Mean motion
4.11025 °/min
Orbital period
87.59 mins
BSTAR
0.00055836
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