ICEYE-X35, 58302
Orbit data source: Space-Track
ICEYE-X35, 58302 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Sat, 11 Nov 2023 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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58302 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FI / FINRelated business
Manufacturer
ICEYE
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-X35
1 58302U 23174AY 25289.19732039 .00032810 00000-0 99186-3 0 9995
2 58302 97.4039 5.2570 0012238 358.3483 1.7717 15.34082299107724Epoch: 2025-10-16T04:44Z
TLE epoch observation values (Epoch: 2025-10-16T04:44:08.481Z)
Latitude
-0.00006°
Longitude
-90.73883°
Altitude
458.386 km
Speed
7.642 km/s
True Right ascension
00h 21m 01s
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
12:42:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.964 km
Perigee altitude
452.225 km
Semi-major axis
6,838.732 km
Eccentricity
0.00122
Inclination
97.4039°
RAAN
5.257°
Arg. of periapsis
358.3483°
True anomaly
1.77604°
Mean anomaly
1.7717°
Eccentric anomaly
1.77387°
Mean motion
3.83778 °/min
Orbital period
93.8 mins
BSTAR
0.00099186
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Other satellites on launch #174 in the year 2023 (2023-11-11 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-X35 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-17 04:22:24.489Z | 105.239° ESE | 2025-10-17 04:24:24.489Z | 65.336° ENE | 16.429° | 2025-10-17 04:26:24.489Z | 28.25° NE |
| 4 mins | 2025-10-17 05:55:24.489Z | 223.2° SW | 2025-10-17 05:57:24.489Z | 273.013° WNW | 21.481° | 2025-10-17 05:59:24.489Z | 313.893° NW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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