Showing default

ICEYE-X25, 56963

Orbit data source: Space-Track

ICEYE-X25, 56963 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Mon, 12 Jun 2023 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.

Not visible in the next 10 days
Identifier
56963, 2023-084AH
Orbit
SSO
Country
Flag of FIFI / FIN
Related business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
90 kg wet, 89 kg dry
Launch date (UTC)
2023-06-12 (3 years 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
0.825 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-X25
1 56963U 23084AH  26140.65349352  .00029435  00000-0  39467-3 0  9991
2 56963  97.5864 285.0575 0002927  60.0235 300.1310 15.57923961163688
Epoch: 2026-05-20T15:41Z
TLE epoch observation values (Epoch: 2026-05-20T15:41:01.840Z)
Latitude
-0.00003°
Longitude
171.48988°
Altitude
395.808 km
Speed
7.673 km/s
True Right ascension
19h 00m 13s
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
07:30:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
392.571 km
Perigee altitude
388.609 km
Semi-major axis
6,768.727 km
Eccentricity
0.00029
Inclination
97.5864°
RAAN
285.0575°
Arg. of periapsis
60.0235°
True anomaly
300.10199°
Mean anomaly
300.131°
Eccentric anomaly
300.11649°
Mean motion
3.89747 °/min
Orbital period
92.37 mins
BSTAR
0.00039467
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
|