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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, 1.6 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   25289.58349749  .00009350  00000-0  59538-3 0  9993
2 59100  97.8116  62.7518 0002910 178.8656 181.2579 15.08988767 74880
Epoch: 2025-10-16T14:00Z
TLE epoch observation values (Epoch: 2025-10-16T14:00:14.183Z)
Latitude
-0.00001°
Longitude
-172.64843°
Altitude
544.365 km
Speed
7.589 km/s
True Right ascension
04h 11m 00s
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
21:14:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.299 km
Perigee altitude
534.275 km
Semi-major axis
6,914.424 km
Eccentricity
0.00029
Inclination
97.8116°
RAAN
62.7518°
Arg. of periapsis
178.8656°
True anomaly
181.25717°
Mean anomaly
181.2579°
Eccentric anomaly
181.25753°
Mean motion
3.77493 °/min
Orbital period
95.37 mins
BSTAR
0.00059538
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