ICEYE-X37, 59102
Orbit data source: Space-Track
ICEYE-X37, 59102 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.
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59102 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
ICEYE US
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, 1.6 m
Radar Cross Section
0.825 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ICEYE-X37
1 59102U 24043E 26130.17421281 .00002810 00000-0 19779-3 0 9995
2 59102 97.8264 266.5997 0016578 135.2409 225.0158 15.05804545119360Epoch: 2026-05-10T04:10Z
TLE epoch observation values (Epoch: 2026-05-10T04:10:51.986Z)
Latitude
-0.00005°
Longitude
-24.09798°
Altitude
560.225 km
Speed
7.577 km/s
True Right ascension
17h 46m 23s
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
23:01:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
557.519 km
Perigee altitude
534.561 km
Semi-major axis
6,924.177 km
Eccentricity
0.00166
Inclination
97.8264°
RAAN
266.5997°
Arg. of periapsis
135.2409°
True anomaly
224.88163°
Mean anomaly
225.0158°
Eccentric anomaly
224.9487°
Mean motion
3.76696 °/min
Orbital period
95.57 mins
BSTAR
0.00019779
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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-X37 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 | 2026-05-10 22:17:58.382Z | 353.698° N | 2026-05-10 22:19:58.382Z | 302.729° NW | 37.28° | 2026-05-10 22:23:58.382Z | 210.328° SW |
| 5 mins | 2026-05-11 09:01:58.382Z | 159.501° S | 2026-05-11 09:03:58.382Z | 93.256° ESE | 44.416° | 2026-05-11 09:06:58.382Z | 351.183° N |
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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