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: 7 hours ago
TLE from 7 hours ago
0 ICEYE-X37
1 59102U 24043E 25336.25988747 .00007423 00000-0 54408-3 0 9999
2 59102 97.8049 105.8209 0015489 317.6911 42.3119 15.03734594 95461Epoch: 2025-12-02T06:14Z
TLE epoch observation values (Epoch: 2025-12-02T06:14:14.277Z)
Latitude
0.00004°
Longitude
-59.08619°
Altitude
550.513 km
Speed
7.591 km/s
True Right ascension
07h 03m 17s
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
11:11:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.132 km
Perigee altitude
541.663 km
Semi-major axis
6,930.535 km
Eccentricity
0.00155
Inclination
97.8049°
RAAN
105.8209°
Arg. of periapsis
317.6911°
True anomaly
42.43155°
Mean anomaly
42.3119°
Eccentric anomaly
42.37171°
Mean motion
3.76178 °/min
Orbital period
95.7 mins
BSTAR
0.00054408
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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 | 2025-12-02 21:10:59.646Z | 33.907° NE | 2025-12-02 21:13:59.646Z | 94.777° ESE | 31.017° | 2025-12-02 21:16:59.646Z | 161.02° S |
| 4 mins | 2025-12-03 07:56:59.646Z | 104.308° ESE | 2025-12-03 07:58:59.646Z | 65.72° ENE | 19.545° | 2025-12-03 08:00:59.646Z | 29.041° NE |
| 4 mins | 2025-12-03 09:31:59.646Z | 226.712° WSW | 2025-12-03 09:33:59.646Z | 276.199° WNW | 24.114° | 2025-12-03 09:35:59.646Z | 313.977° NW |
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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