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: 22 hours ago
TLE from 22 hours ago
0 ICEYE-X31
1 58288U 23174AJ 26172.50616256 .00014176 00000-0 42733-3 0 9998
2 58288 97.3777 248.2459 0000885 313.2598 46.8571 15.34421401145410Epoch: 2026-06-21T12:08Z
TLE epoch observation values (Epoch: 2026-06-21T12:08:52.445Z)
Latitude
-0.00001°
Longitude
156.32192°
Altitude
465.336 km
Speed
7.634 km/s
True Right ascension
16h 32m 59s
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
21:38:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.19 km
Perigee altitude
458.98 km
Semi-major axis
6,837.722 km
Eccentricity
0.00009
Inclination
97.3777°
RAAN
248.2459°
Arg. of periapsis
313.2598°
True anomaly
46.8645°
Mean anomaly
46.8571°
Eccentric anomaly
46.8608°
Mean motion
3.83863 °/min
Orbital period
93.78 mins
BSTAR
0.00042733
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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 | 2026-06-22 18:27:56.154Z | 326.705° NNW | 2026-06-22 18:28:56.154Z | 294.471° NW | 28.493° | 2026-06-22 18:31:56.154Z | 224.217° SW |
| 5 mins | 2026-06-23 04:58:56.154Z | 154.087° SSE | 2026-06-23 05:00:56.154Z | 85.668° E | 42.446° | 2026-06-23 05:03:56.154Z | 354.983° N |
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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