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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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: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X36
1 59103U 24043F 26034.25942652 .00008255 00000-0 57849-3 0 9997
2 59103 97.8151 170.2640 0006470 58.6037 301.5821 15.05464569104984Epoch: 2026-02-03T06:13Z
TLE epoch observation values (Epoch: 2026-02-03T06:13:34.451Z)
Latitude
-0.00003°
Longitude
-56.57247°
Altitude
550.793 km
Speed
7.588 km/s
True Right ascension
11h 21m 03s
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
13:56:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
551.564 km
Perigee altitude
542.602 km
Semi-major axis
6,925.22 km
Eccentricity
0.00065
Inclination
97.8151°
RAAN
170.264°
Arg. of periapsis
58.6037°
True anomaly
301.51891°
Mean anomaly
301.5821°
Eccentric anomaly
301.55051°
Mean motion
3.76611 °/min
Orbital period
95.59 mins
BSTAR
0.00057849
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-03 21:09:56.252Z | 46.381° ENE | 2026-02-03 21:11:56.252Z | 84.234° E | 23.766° | 2026-02-03 21:14:56.252Z | 147.679° SSE |
| 5 mins | 2026-02-04 09:28:56.252Z | 205.892° SW | 2026-02-04 09:30:56.252Z | 256.726° W | 31.088° | 2026-02-04 09:33:56.252Z | 325.151° NNW |
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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