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: 13 hours ago
TLE from 13 hours ago
0 ICEYE-X36
1 59103U 24043F 26175.15667573 .00002775 00000-0 19019-3 0 9996
2 59103 97.8368 313.3511 0004582 302.6860 57.3925 15.06905337126191Epoch: 2026-06-24T03:45Z
TLE epoch observation values (Epoch: 2026-06-24T03:45:36.783Z)
Latitude
0.00005°
Longitude
-15.3701°
Altitude
547.014 km
Speed
7.589 km/s
True Right ascension
20h 53m 24s
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
03:42:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
545.836 km
Perigee altitude
539.494 km
Semi-major axis
6,920.802 km
Eccentricity
0.00046
Inclination
97.8368°
RAAN
313.3511°
Arg. of periapsis
302.686°
True anomaly
57.43674°
Mean anomaly
57.3925°
Eccentric anomaly
57.41462°
Mean motion
3.76971 °/min
Orbital period
95.5 mins
BSTAR
0.00019019
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-24 21:51:16.916Z | 23.295° NE | 2026-06-24 21:54:16.916Z | 74.981° E | 38.318° | 2026-06-24 21:58:16.916Z | 178.445° S |
| 5 mins | 2026-06-25 08:36:16.916Z | 111.966° ESE | 2026-06-25 08:38:16.916Z | 63.162° ENE | 25.175° | 2026-06-25 08:41:16.916Z | 11.693° NNE |
| 4 mins | 2026-06-25 10:11:16.916Z | 238.578° WSW | 2026-06-25 10:12:16.916Z | 257.764° W | 18.036° | 2026-06-25 10:15:16.916Z | 310.167° 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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