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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Edit Public Description
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: 12 hours ago
TLE from 12 hours ago
0 ICEYE-X37
1 59102U 24043E 25289.60312070 .00005301 00000-0 39669-3 0 9990
2 59102 97.8014 58.7807 0017280 111.8427 248.4637 15.03063680 88456Epoch: 2025-10-16T14:28Z
TLE epoch observation values (Epoch: 2025-10-16T14:28:29.628Z)
Latitude
-0.0001°
Longitude
176.29679°
Altitude
564.93 km
Speed
7.576 km/s
True Right ascension
03h 55m 07s
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
21:14:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
566.441 km
Perigee altitude
542.482 km
Semi-major axis
6,932.598 km
Eccentricity
0.00173
Inclination
97.8014°
RAAN
58.7807°
Arg. of periapsis
111.8427°
True anomaly
248.27966°
Mean anomaly
248.4637°
Eccentric anomaly
248.37166°
Mean motion
3.7601 °/min
Orbital period
95.74 mins
BSTAR
0.00039669
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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 | 2025-10-17 08:11:21.156Z | 131.076° SE | 2025-10-17 08:14:21.156Z | 65.562° ENE | 29.015° | 2025-10-17 08:17:21.156Z | 9.221° NNE |
| 6 mins | 2025-10-17 21:24:21.156Z | 23.895° NE | 2025-10-17 21:27:21.156Z | 120.255° SE | 40.589° | 2025-10-17 21:30:21.156Z | 179.874° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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