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: 19 hours ago
TLE from 19 hours ago
0 ICEYE-X36
1 59103U 24043F 25289.32503972 .00005629 00000-0 41541-3 0 9998
2 59103 97.8064 59.1110 0006736 68.7201 291.4743 15.03662972 88453Epoch: 2025-10-16T07:48Z
TLE epoch observation values (Epoch: 2025-10-16T07:48:03.431Z)
Latitude
-0.00002°
Longitude
-82.98968°
Altitude
556.962 km
Speed
7.584 km/s
True Right ascension
03h 56m 26s
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
21:14:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
557.287 km
Perigee altitude
547.949 km
Semi-major axis
6,930.755 km
Eccentricity
0.00067
Inclination
97.8064°
RAAN
59.111°
Arg. of periapsis
68.7201°
True anomaly
291.40245°
Mean anomaly
291.4743°
Eccentric anomaly
291.43838°
Mean motion
3.7616 °/min
Orbital period
95.7 mins
BSTAR
0.00041541
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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 | 2025-10-17 07:54:21.494Z | 113.32° SE | 2025-10-17 07:57:21.494Z | 59.409° ENE | 19.117° | 2025-10-17 07:59:21.494Z | 25.41° NE |
| 5 mins | 2025-10-17 09:29:21.494Z | 215.522° SW | 2025-10-17 09:31:21.494Z | 256.546° W | 24.439° | 2025-10-17 09:34:21.494Z | 317.214° NNW |
| 5 mins | 2025-10-17 21:07:21.494Z | 46.157° ENE | 2025-10-17 21:09:21.494Z | 94.754° ESE | 28.943° | 2025-10-17 21:12:21.494Z | 158.448° S |
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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