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: 14 hours ago
TLE from 14 hours ago
0 ICEYE-X31
1 58288U 23174AJ 25289.18330355 .00019014 00000-0 76078-3 0 9998
2 58288 97.4058 1.2248 0004020 109.4035 250.7638 15.25117376107446Epoch: 2025-10-16T04:23Z
TLE epoch observation values (Epoch: 2025-10-16T04:23:57.426Z)
Latitude
-0.00001°
Longitude
-89.71116°
Altitude
494.441 km
Speed
7.617 km/s
True Right ascension
00h 04m 53s
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
12:47:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.152 km
Perigee altitude
484.632 km
Semi-major axis
6,865.529 km
Eccentricity
0.0004
Inclination
97.4058°
RAAN
1.2248°
Arg. of periapsis
109.4035°
True anomaly
250.72031°
Mean anomaly
250.7638°
Eccentric anomaly
250.74206°
Mean motion
3.81533 °/min
Orbital period
94.36 mins
BSTAR
0.00076078
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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 | 2025-10-17 04:10:04.560Z | 114.229° SE | 2025-10-17 04:12:04.560Z | 76.804° E | 19.26° | 2025-10-17 04:14:04.560Z | 33.414° NE |
| 4 mins | 2025-10-17 05:44:04.560Z | 226.572° WSW | 2025-10-17 05:46:04.560Z | 271.55° WNW | 20.283° | 2025-10-17 05:48:04.560Z | 310.573° NW |
| 4 mins | 2025-10-17 17:12:04.560Z | 51.825° ENE | 2025-10-17 17:14:04.560Z | 103.479° ESE | 24.77° | 2025-10-17 17:16:04.560Z | 147.866° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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