Showing default

ICEYE-X46, 63258

Orbit data source: Space-Track

ICEYE-X46, 63258 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Sat, 15 Mar 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
63258, 2025-052BA
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)
2025-03-15 (1 year 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: 11 hours ago

TLE from 11 hours ago
0 ICEYE-X46
1 63258U 25052BA  26219.67920818  .00000561  00000-0  55865-4 0  9994
2 63258  97.6821 110.5711 0001533  84.3458 275.7937 14.95435910 76340
Epoch: 2026-08-07T16:18Z
TLE epoch observation values (Epoch: 2026-08-07T16:18:03.586Z)
Latitude
-0.00012°
Longitude
-90.14527°
Altitude
583.961 km
Speed
7.568 km/s
True Right ascension
07h 22m 17s
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
17:38:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.097 km
Perigee altitude
576.964 km
Semi-major axis
6,956.168 km
Eccentricity
0.00015
Inclination
97.6821°
RAAN
110.5711°
Arg. of periapsis
84.3458°
True anomaly
275.77622°
Mean anomaly
275.7937°
Eccentric anomaly
275.78496°
Mean motion
3.741 °/min
Orbital period
96.23 mins
BSTAR
0.000055865
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
|