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: 10 hours ago
TLE from 10 hours ago
0 ICEYE-X31
1 58288U 23174AJ 26023.83885287 .00020662 00000-0 72989-3 0 9994
2 58288 97.3936 100.0606 0003618 112.6840 247.4783 15.29227848122652Epoch: 2026-01-23T20:07Z
TLE epoch observation values (Epoch: 2026-01-23T20:07:56.887Z)
Latitude
-0.00005°
Longitude
34.90166°
Altitude
482.174 km
Speed
7.624 km/s
True Right ascension
06h 40m 14s
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
07:33:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.552 km
Perigee altitude
472.593 km
Semi-major axis
6,853.209 km
Eccentricity
0.00036
Inclination
97.3936°
RAAN
100.0606°
Arg. of periapsis
112.684°
True anomaly
247.44001°
Mean anomaly
247.4783°
Eccentric anomaly
247.45915°
Mean motion
3.82562 °/min
Orbital period
94.1 mins
BSTAR
0.00072989
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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 | 2026-01-24 17:07:52.511Z | 54.385° ENE | 2026-01-24 17:09:52.511Z | 99.711° ESE | 20.854° | 2026-01-24 17:11:52.511Z | 141.342° SSE |
| 5 mins | 2026-01-25 05:14:52.511Z | 186.774° SSW | 2026-01-25 05:16:52.511Z | 246.282° WSW | 39.504° | 2026-01-25 05:19:52.511Z | 336.858° NNW |
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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