Showing default

ICEYE-X52, 64572

Orbit data source: Space-Track

ICEYE-X52, 64572 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Mon, 23 Jun 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
64572, 2025-135AW
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)
2025-06-23 (8 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 2.4 m
Radar Cross Section
0.776 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-X52
1 64572U 25135AW  26062.47004490  .00004050  00000-0  39413-3 0  9996
2 64572  97.7617 177.9983 0001292  10.9036 349.2212 14.93088573 38103
Epoch: 2026-03-03T11:16Z
TLE epoch observation values (Epoch: 2026-03-03T11:16:51.879Z)
Latitude
0.00006°
Longitude
-152.46652°
Altitude
590.471 km
Speed
7.565 km/s
True Right ascension
11h 51m 59s
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
21:50:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.229 km
Perigee altitude
584.43 km
Semi-major axis
6,963.466 km
Eccentricity
0.00013
Inclination
97.7617°
RAAN
177.9983°
Arg. of periapsis
10.9036°
True anomaly
349.21843°
Mean anomaly
349.2212°
Eccentric anomaly
349.21982°
Mean motion
3.73512 °/min
Orbital period
96.38 mins
BSTAR
0.00039413
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
|