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: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X37
1 59102U 24043E 26286.94068532 .00004546 00000-0 30858-3 0 9997
2 59102 97.8480 65.9937 0014361 330.6660 29.3759 15.06853319142961Epoch: 2026-10-13T22:34Z
TLE epoch observation values (Epoch: 2026-10-13T22:34:35.211Z)
Latitude
-0.00004°
Longitude
64.84945°
Altitude
540.219 km
Speed
7.597 km/s
True Right ascension
04h 23m 58s
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
23:24:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
552.764 km
Perigee altitude
532.886 km
Semi-major axis
6,920.962 km
Eccentricity
0.00144
Inclination
97.848°
RAAN
65.9937°
Arg. of periapsis
330.666°
True anomaly
29.45675°
Mean anomaly
29.3759°
Eccentric anomaly
29.41631°
Mean motion
3.76958 °/min
Orbital period
95.5 mins
BSTAR
0.00030858
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-14 09:52:23.786Z | 204.578° SW | 2026-10-14 09:54:23.786Z | 263.553° W | 40.95° | 2026-10-14 09:57:23.786Z | 328.628° NNW |
| 4 mins | 2026-10-14 21:29:23.786Z | 65.694° ENE | 2026-10-14 21:30:23.786Z | 85.831° E | 21.587° | 2026-10-14 21:33:23.786Z | 141.54° SSE |
| 5 mins | 2026-10-14 23:03:23.786Z | 332.515° NNW | 2026-10-14 23:05:23.786Z | 289.65° WNW | 26.07° | 2026-10-14 23:08:23.786Z | 235.986° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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