ICEYE-X36, 59103
Orbit data source: Space-Track
ICEYE-X36, 59103 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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59103 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: 15 hours ago
TLE from 15 hours ago
0 ICEYE-X36
1 59103U 24043F 26235.56777850 .00002845 00000-0 19183-3 0 9998
2 59103 97.8448 14.8979 0007509 93.6534 266.5552 15.07480051135291Epoch: 2026-08-23T13:37Z
TLE epoch observation values (Epoch: 2026-08-23T13:37:36.062Z)
Latitude
-0.00001°
Longitude
-161.36433°
Altitude
547.28 km
Speed
7.588 km/s
True Right ascension
00h 59m 35s
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
19:32:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
546.101 km
Perigee altitude
535.71 km
Semi-major axis
6,919.042 km
Eccentricity
0.00075
Inclination
97.8448°
RAAN
14.8979°
Arg. of periapsis
93.6534°
True anomaly
266.46931°
Mean anomaly
266.5552°
Eccentric anomaly
266.51226°
Mean motion
3.77115 °/min
Orbital period
95.46 mins
BSTAR
0.00019183
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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-X36 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 | 2026-08-24 08:52:55.228Z | 133.53° SE | 2026-08-24 08:55:55.228Z | 63.558° ENE | 30.401° | 2026-08-24 08:58:55.228Z | 7.117° NNE |
| 6 mins | 2026-08-24 22:03:55.228Z | 24.952° NE | 2026-08-24 22:05:55.228Z | 64.03° ENE | 39.465° | 2026-08-24 22:09:55.228Z | 181.477° SSW |
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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