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.

Not visible in the next 10 days
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, 2.4 m
Radar Cross Section
1.837 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 ICEYE-X21
1 55049U 23001AS  26115.48897468  .00138340  00000-0  53573-3 0  9993
2 55049  97.3282 197.4655 0004908 224.0743 136.0137 15.86836034185218
Epoch: 2026-04-25T11:44Z
TLE epoch observation values (Epoch: 2026-04-25T11:44:07.412Z)
Latitude
-0.00008°
Longitude
167.92801°
Altitude
316.706 km
Speed
7.717 km/s
True Right ascension
13h 09m 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
01:44:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
311.315 km
Perigee altitude
304.752 km
Semi-major axis
6,686.171 km
Eccentricity
0.00049
Inclination
97.3282°
RAAN
197.4655°
Arg. of periapsis
224.0743°
True anomaly
136.05274°
Mean anomaly
136.0137°
Eccentric anomaly
136.03322°
Mean motion
3.96988 °/min
Orbital period
90.68 mins
BSTAR
0.00053573
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|