Showing default

ICEYE-X36, 59103

Orbit data source: Space-Track

ICEYE-X36, 59103 is a payload satellite owned by ICEYE US (US) in SSO that was launched on Mon, 04 Mar 2024 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
59103, 2024-043F
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
ICEYE US
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
90 kg wet, 89 kg dry
Launch date (UTC)
2024-03-04 (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: 8 hours ago

TLE from 8 hours ago
0 ICEYE-X36
1 59103U 24043F   26082.37017399  .00006319  00000-0  43641-3 0  9998
2 59103  97.8235 219.0403 0004820 241.2258 118.8484 15.06112893112229
Epoch: 2026-03-23T08:53Z
TLE epoch observation values (Epoch: 2026-03-23T08:53:03.032Z)
Latitude
-0.0001°
Longitude
-95.08548°
Altitude
552.763 km
Speed
7.585 km/s
True Right ascension
14h 36m 09s
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
22:26:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
548.431 km
Perigee altitude
541.757 km
Semi-major axis
6,923.231 km
Eccentricity
0.00048
Inclination
97.8235°
RAAN
219.0403°
Arg. of periapsis
241.2258°
True anomaly
118.89676°
Mean anomaly
118.8484°
Eccentric anomaly
118.87258°
Mean motion
3.76773 °/min
Orbital period
95.55 mins
BSTAR
0.00043641
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
|