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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ICEYE-X31 radio frequencies
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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: 15 hours ago
TLE from 15 hours ago
0 ICEYE-X31
1 58288U 23174AJ 25258.52958742 .00015376 00000-0 64045-3 0 9996
2 58288 97.4092 330.9256 0003145 192.4318 167.6842 15.23814381102770Epoch: 2025-09-15T12:42Z
TLE epoch observation values (Epoch: 2025-09-15T12:42:36.353Z)
Latitude
-0.00001°
Longitude
145.5412°
Altitude
499.555 km
Speed
7.614 km/s
True Right ascension
22h 03m 42s
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
20:35:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.469 km
Perigee altitude
489.148 km
Semi-major axis
6,869.446 km
Eccentricity
0.00031
Inclination
97.4092°
RAAN
330.9256°
Arg. of periapsis
192.4318°
True anomaly
167.69188°
Mean anomaly
167.6842°
Eccentric anomaly
167.68804°
Mean motion
3.81207 °/min
Orbital period
94.44 mins
BSTAR
0.00064045
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-16 04:35:53.632Z | 145.555° SSE | 2025-09-16 04:38:53.632Z | 81.587° E | 35.139° | 2025-09-16 04:41:53.632Z | 4.315° NNE |
| 7 mins | 2025-09-16 17:37:53.632Z | 17.335° NNE | 2025-09-16 17:41:53.632Z | 148.458° SSE | 40.596° | 2025-09-16 17:44:53.632Z | 184.638° SSW |
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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