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: 9 hours ago
TLE from 9 hours ago
0 ICEYE-X37
1 59102U 24043E 26255.33005509 .00003057 00000-0 20978-3 0 9999
2 59102 97.8434 33.7946 0016362 75.7301 284.5742 15.06679303138203Epoch: 2026-09-12T07:55Z
TLE epoch observation values (Epoch: 2026-09-12T07:55:16.759Z)
Latitude
0.00001°
Longitude
-76.36584°
Altitude
546.581 km
Speed
7.59 km/s
True Right ascension
02h 15m 10s
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
09:07:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
554.683 km
Perigee altitude
532.033 km
Semi-major axis
6,921.495 km
Eccentricity
0.00164
Inclination
97.8434°
RAAN
33.7946°
Arg. of periapsis
75.7301°
True anomaly
284.39265°
Mean anomaly
284.5742°
Eccentric anomaly
284.48343°
Mean motion
3.76915 °/min
Orbital period
95.51 mins
BSTAR
0.00020978
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-12 21:15:30.936Z | 55.775° ENE | 2026-09-12 21:17:30.936Z | 88.569° E | 16.932° | 2026-09-12 21:19:30.936Z | 124.503° SE |
| 5 mins | 2026-09-12 22:50:30.936Z | 336.984° NNW | 2026-09-12 22:52:30.936Z | 287.516° WNW | 31.779° | 2026-09-12 22:55:30.936Z | 228.833° WSW |
| 6 mins | 2026-09-13 09:33:30.936Z | 181.984° SSW | 2026-09-13 09:35:30.936Z | 222.882° SW | 57.946° | 2026-09-13 09:39:30.936Z | 340.224° N |
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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