ICEYE-X46, 63258
Orbit data source: Space-Track
ICEYE-X46, 63258 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Sat, 15 Mar 2025 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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63258 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
80 kg wet, 80 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 2.4 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 ICEYE-X46
1 63258U 25052BA 26074.27074610 .00002376 00000-0 22090-3 0 9998
2 63258 97.7007 327.9058 0001780 77.2866 282.8554 14.95279637 54615Epoch: 2026-03-15T06:29Z
TLE epoch observation values (Epoch: 2026-03-15T06:29:52.463Z)
Latitude
0.00003°
Longitude
57.55722°
Altitude
584.278 km
Speed
7.568 km/s
True Right ascension
21h 51m 37s
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
05:42:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.755 km
Perigee altitude
577.278 km
Semi-major axis
6,956.654 km
Eccentricity
0.00018
Inclination
97.7007°
RAAN
327.9058°
Arg. of periapsis
77.2866°
True anomaly
282.83551°
Mean anomaly
282.8554°
Eccentric anomaly
282.84546°
Mean motion
3.74061 °/min
Orbital period
96.24 mins
BSTAR
0.0002209
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Other satellites on launch #52 in the year 2025 (2025-03-15 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-X46 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-16 05:32:55.578Z | 18.892° NNE | 2026-03-16 05:35:55.578Z | 58.294° ENE | 41.208° | 2026-03-16 05:39:55.578Z | 183.813° SSW |
| 6 mins | 2026-03-16 16:21:55.578Z | 133.704° SE | 2026-03-16 16:24:55.578Z | 62.185° ENE | 31.807° | 2026-03-16 16:27:55.578Z | 6.878° NNE |
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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