ICEYE-X31, 58288
Orbit data source: Space-Track
ICEYE-X31, 58288 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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58288 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-X31
1 58288U 23174AJ 25290.29867589 .00022416 00000-0 89491-3 0 9999
2 58288 97.4060 2.3283 0003939 106.2943 253.8728 15.25158598107615Epoch: 2025-10-17T07:10Z
TLE epoch observation values (Epoch: 2025-10-17T07:10:05.596Z)
Latitude
-0.00009°
Longitude
-131.24105°
Altitude
494.159 km
Speed
7.617 km/s
True Right ascension
00h 09m 18s
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
15:01:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.972 km
Perigee altitude
484.564 km
Semi-major axis
6,865.405 km
Eccentricity
0.00039
Inclination
97.406°
RAAN
2.3283°
Arg. of periapsis
106.2943°
True anomaly
253.82944°
Mean anomaly
253.8728°
Eccentric anomaly
253.85112°
Mean motion
3.81543 °/min
Orbital period
94.35 mins
BSTAR
0.00089491
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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-X31 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 | 2025-10-18 05:21:28.471Z | 205.11° SW | 2025-10-18 05:23:28.471Z | 280.163° WNW | 33.27° | 2025-10-18 05:26:28.471Z | 333.774° NNW |
| 4 mins | 2025-10-18 18:23:28.471Z | 324.366° NNW | 2025-10-18 18:24:28.471Z | 295.638° NW | 26.543° | 2025-10-18 18:27:28.471Z | 228.864° WSW |
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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