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: 18 hours ago
TLE from 18 hours ago
0 ICEYE-X37
1 59102U 24043E 26175.15647955 .00002455 00000-0 17186-3 0 9995
2 59102 97.8312 312.2670 0014704 351.4448 8.6525 15.06157135126138Epoch: 2026-06-24T03:45Z
TLE epoch observation values (Epoch: 2026-06-24T03:45:19.833Z)
Latitude
-0.00005°
Longitude
-16.38337°
Altitude
540.945 km
Speed
7.597 km/s
True Right ascension
20h 49m 04s
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
08:37:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
555.139 km
Perigee altitude
534.779 km
Semi-major axis
6,923.096 km
Eccentricity
0.00147
Inclination
97.8312°
RAAN
312.267°
Arg. of periapsis
351.4448°
True anomaly
8.67789°
Mean anomaly
8.6525°
Eccentric anomaly
8.66519°
Mean motion
3.76784 °/min
Orbital period
95.55 mins
BSTAR
0.00017186
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-24 21:51:24.290Z | 20.206° NNE | 2026-06-24 21:54:24.290Z | 63.923° ENE | 40.337° | 2026-06-24 21:58:24.290Z | 182.39° SSW |
| 5 mins | 2026-06-25 08:36:24.290Z | 121.481° SE | 2026-06-25 08:38:24.290Z | 74.339° E | 27.76° | 2026-06-25 08:41:24.290Z | 12.205° 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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