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ICEYE-X38, 59100

Orbit data source: Space-Track

ICEYE-X38, 59100 is a payload satellite owned by ICEYE (FI) 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.

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Identifier
59100, 2024-043C
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)
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, 2.4 m
Radar Cross Section
0.825 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 ICEYE-X38
1 59100U 24043C   26175.26069399  .00004093  00000-0  23635-3 0  9991
2 59100  97.8409 319.2023 0003780  73.9600 286.2046 15.12910603112748
Epoch: 2026-06-24T06:15Z
TLE epoch observation values (Epoch: 2026-06-24T06:15:23.960Z)
Latitude
-0.00005°
Longitude
-47.06798°
Altitude
529.669 km
Speed
7.598 km/s
True Right ascension
21h 16m 48s
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
06:17:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.933 km
Perigee altitude
521.714 km
Semi-major axis
6,902.46 km
Eccentricity
0.00038
Inclination
97.8409°
RAAN
319.2023°
Arg. of periapsis
73.96°
True anomaly
286.163°
Mean anomaly
286.2046°
Eccentric anomaly
286.1838°
Mean motion
3.78475 °/min
Orbital period
95.12 mins
BSTAR
0.00023635
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