Showing default

ICEYE-X21, 55049

Orbit data source: Space-Track

ICEYE-X21, 55049 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Tue, 03 Jan 2023 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.

Loading next visibility...
Identifier
55049, 2023-001AS
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)
2023-01-03 (3 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: 15 hours ago

TLE from 15 hours ago
0 ICEYE-X21
1 55049U 23001AS  26022.50615925  .00107434  00000-0  10332-2 0  9994
2 55049  97.3490  98.9627 0010481 228.8855 131.1501 15.66158513170562
Epoch: 2026-01-22T12:08Z
TLE epoch observation values (Epoch: 2026-01-22T12:08:52.159Z)
Latitude
-0.00002°
Longitude
154.88703°
Altitude
377.723 km
Speed
7.68 km/s
True Right ascension
06h 35m 51s
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
03:56:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
373.88 km
Perigee altitude
359.742 km
Semi-major axis
6,744.948 km
Eccentricity
0.00105
Inclination
97.349°
RAAN
98.9627°
Arg. of periapsis
228.8855°
True anomaly
131.24046°
Mean anomaly
131.1501°
Eccentric anomaly
131.19529°
Mean motion
3.9181 °/min
Orbital period
91.88 mins
BSTAR
0.0010332
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|