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: 15 hours ago
TLE from 15 hours ago
0 ICEYE-X38
1 59100U 24043C 26235.56983330 .00003940 00000-0 22480-3 0 9998
2 59100 97.8484 21.2312 0002295 178.0870 182.0370 15.13374328121863Epoch: 2026-08-23T13:40Z
TLE epoch observation values (Epoch: 2026-08-23T13:40:33.597Z)
Latitude
0.00006°
Longitude
-155.77279°
Altitude
530.571 km
Speed
7.597 km/s
True Right ascension
01h 24m 55s
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
19:32:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
524.496 km
Perigee altitude
521.329 km
Semi-major axis
6,901.049 km
Eccentricity
0.00023
Inclination
97.8484°
RAAN
21.2312°
Arg. of periapsis
178.087°
True anomaly
182.03607°
Mean anomaly
182.037°
Eccentric anomaly
182.03653°
Mean motion
3.78591 °/min
Orbital period
95.09 mins
BSTAR
0.0002248
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-24 08:52:26.747Z | 106.019° ESE | 2026-08-24 08:54:26.747Z | 71.297° E | 17.103° | 2026-08-24 08:56:26.747Z | 34.051° NE |
| 5 mins | 2026-08-24 10:26:26.747Z | 212.508° SW | 2026-08-24 10:28:26.747Z | 257.25° W | 26.034° | 2026-08-24 10:31:26.747Z | 320.319° NNW |
| 4 mins | 2026-08-24 22:00:26.747Z | 59.042° ENE | 2026-08-24 22:02:26.747Z | 107.059° ESE | 22.63° | 2026-08-24 22:04:26.747Z | 145.441° SSE |
| 4 mins | 2026-08-24 23:34:26.747Z | 325.352° NNW | 2026-08-24 23:36:26.747Z | 283.969° WNW | 19.134° | 2026-08-24 23:38:26.747Z | 248.353° W |
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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