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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59100 intel report (Beta)
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Identifier
Orbit
Country
FI / FINRelated business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
90 kg wet, 89 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X38
1 59100U 24043C 26248.33037277 .00002439 00000-0 14030-3 0 9991
2 59100 97.8509 34.3706 0003207 143.7684 216.3764 15.13470886123797Epoch: 2026-09-05T07:55Z
TLE epoch observation values (Epoch: 2026-09-05T07:55:44.207Z)
Latitude
-0.00001°
Longitude
-69.00498°
Altitude
530.476 km
Speed
7.597 km/s
True Right ascension
02h 17m 28s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
06:05:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
524.832 km
Perigee altitude
520.406 km
Semi-major axis
6,900.756 km
Eccentricity
0.00032
Inclination
97.8509°
RAAN
34.3706°
Arg. of periapsis
143.7684°
True anomaly
216.35461°
Mean anomaly
216.3764°
Eccentric anomaly
216.3655°
Mean motion
3.78615 °/min
Orbital period
95.08 mins
BSTAR
0.0001403
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Other satellites on launch #43 in the year 2024 (2024-03-04 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ICEYE-X38 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-05 22:46:20.823Z | 10.536° NNE | 2026-09-05 22:49:20.823Z | 318.533° NNW | 44.708° | 2026-09-05 22:52:20.823Z | 196.543° SSW |
| 5 mins | 2026-09-06 09:28:20.823Z | 127.292° SE | 2026-09-06 09:30:20.823Z | 55.814° ENE | 33.594° | 2026-09-06 09:33:20.823Z | 2.566° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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