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ICEYE-X11, 48918

Orbit data source: Space-Track

ICEYE-X11, 48918 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). 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
48918, 2021-059AR
Orbit
SSO
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)
2021-06-30 (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, 2.4 m
Radar Cross Section
1.837 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 ICEYE-X11
1 48918U 21059AR  26172.49481542  .00363307  62025-4  54578-3 0  9995
2 48918  97.6238  12.5684 0002338 240.8676 119.2370 16.04707218278682
Epoch: 2026-06-21T11:52Z
TLE epoch observation values (Epoch: 2026-06-21T11:52:32.052Z)
Latitude
-0.00003°
Longitude
-75.25942°
Altitude
265.359 km
Speed
7.747 km/s
True Right ascension
00h 50m 16s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
21:38:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
259.818 km
Perigee altitude
256.715 km
Semi-major axis
6,636.403 km
Eccentricity
0.00023
Inclination
97.6238°
RAAN
12.5684°
Arg. of periapsis
240.8676°
True anomaly
119.26038°
Mean anomaly
119.237°
Eccentric anomaly
119.24869°
Mean motion
4.01462 °/min
Orbital period
89.67 mins
BSTAR
0.00054578
Loading maneuver chart data...
Computing Atmospheric mass density...

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