Showing default

ICEYE-X26, 56961

Orbit data source: Space-Track

ICEYE-X26, 56961 is a payload satellite owned by ICEYE US (US) 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
56961, 2023-084AF
Orbit
SSO
Country
Flag of USUS
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 (2 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, 1.6 m
Radar Cross Section
0.825 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 ICEYE-X26
1 56961U 23084AF  25334.34349851  .00043151  00000-0  49005-3 0  9993
2 56961  97.5727 117.1774 0000010 107.0533 253.0725 15.62229028137949
Epoch: 2025-11-30T08:14Z
TLE epoch observation values (Epoch: 2025-11-30T08:14:38.271Z)
Latitude
-0.00006°
Longitude
-75.94077°
Altitude
384.364 km
Speed
7.679 km/s
True Right ascension
07h 48m 42s
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
21:44:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
378.144 km
Perigee altitude
378.13 km
Semi-major axis
6,756.274 km
Eccentricity
0
Inclination
97.5727°
RAAN
117.1774°
Arg. of periapsis
107.0533°
True anomaly
253.07239°
Mean anomaly
253.0725°
Eccentric anomaly
253.07245°
Mean motion
3.90825 °/min
Orbital period
92.11 mins
BSTAR
0.00049005
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|