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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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, 2.4 m
Radar Cross Section
0.825 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 ICEYE-X31
1 58288U 23174AJ 26126.83388418 .00014449 00000-0 45583-3 0 9998
2 58288 97.3788 202.6301 0003914 115.7304 244.4342 15.32961324138413Epoch: 2026-05-06T20:00Z
TLE epoch observation values (Epoch: 2026-05-06T20:00:47.593Z)
Latitude
-0.00006°
Longitude
37.74311°
Altitude
471.249 km
Speed
7.63 km/s
True Right ascension
13h 30m 31s
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
09:22:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.608 km
Perigee altitude
461.252 km
Semi-major axis
6,842.067 km
Eccentricity
0.00039
Inclination
97.3788°
RAAN
202.6301°
Arg. of periapsis
115.7304°
True anomaly
244.39375°
Mean anomaly
244.4342°
Eccentric anomaly
244.41397°
Mean motion
3.83497 °/min
Orbital period
93.87 mins
BSTAR
0.00045583
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-07 05:33:18.079Z | 209.894° SW | 2026-05-07 05:35:18.079Z | 273.68° WNW | 29.445° | 2026-05-07 05:37:18.079Z | 321.688° NNW |
| 4 mins | 2026-05-07 18:31:18.079Z | 327.046° NNW | 2026-05-07 18:32:18.079Z | 300.835° NW | 24.507° | 2026-05-07 18:35:18.079Z | 231.506° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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