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: 5 hours ago
TLE from 5 hours ago
0 ICEYE-X37
1 59102U 24043E 26036.84808917 .00010878 00000-0 77243-3 0 9992
2 59102 97.8108 172.0701 0016304 94.8720 265.4368 15.04795145105320Epoch: 2026-02-05T20:21Z
TLE epoch observation values (Epoch: 2026-02-05T20:21:14.904Z)
Latitude
0.00002°
Longitude
90.76356°
Altitude
556.11 km
Speed
7.583 km/s
True Right ascension
11h 28m 16s
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
03:12:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
560.433 km
Perigee altitude
537.844 km
Semi-major axis
6,927.275 km
Eccentricity
0.00163
Inclination
97.8108°
RAAN
172.0701°
Arg. of periapsis
94.872°
True anomaly
265.25059°
Mean anomaly
265.4368°
Eccentric anomaly
265.34369°
Mean motion
3.76443 °/min
Orbital period
95.63 mins
BSTAR
0.00077243
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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 | 2026-02-06 09:15:38.675Z | 193.822° SSW | 2026-02-06 09:17:38.675Z | 252.311° W | 37.493° | 2026-02-06 09:20:38.675Z | 332.174° NNW |
| 4 mins | 2026-02-06 20:53:38.675Z | 68.315° E | 2026-02-06 20:54:38.675Z | 87.018° E | 17.213° | 2026-02-06 20:57:38.675Z | 138.083° SSE |
| 5 mins | 2026-02-06 22:27:38.675Z | 337.687° N | 2026-02-06 22:29:38.675Z | 293.155° NW | 26.144° | 2026-02-06 22:32:38.675Z | 232.583° 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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