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: 17 hours ago

TLE from 17 hours ago
0 ICEYE-X25
1 56963U 23084AH  26259.70108845  .00031848  00000-0  30955-3 0  9992
2 56963  97.5982  52.7837 0002795 334.8844  25.2279 15.66251461182274
Epoch: 2026-09-16T16:49Z
TLE epoch observation values (Epoch: 2026-09-16T16:49:34.042Z)
Latitude
-0.00001°
Longitude
164.74295°
Altitude
371.083 km
Speed
7.688 km/s
True Right ascension
03h 31m 08s
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
02:56:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
368.44 km
Perigee altitude
364.67 km
Semi-major axis
6,744.692 km
Eccentricity
0.00028
Inclination
97.5982°
RAAN
52.7837°
Arg. of periapsis
334.8844°
True anomaly
25.24156°
Mean anomaly
25.2279°
Eccentric anomaly
25.23473°
Mean motion
3.91832 °/min
Orbital period
91.88 mins
BSTAR
0.00030955
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|