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: 17 hours ago
TLE from 17 hours ago
0 ICEYE-X46
1 63258U 25052BA 26265.11055572 .00001555 00000-0 14534-3 0 9991
2 63258 97.6743 155.0850 0001744 85.1889 274.9531 14.95550446 83130Epoch: 2026-09-22T02:39Z
TLE epoch observation values (Epoch: 2026-09-22T02:39:12.014Z)
Latitude
-0.00002°
Longitude
114.30421°
Altitude
583.609 km
Speed
7.569 km/s
True Right ascension
10h 20m 20s
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
12:40:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.888 km
Perigee altitude
576.462 km
Semi-major axis
6,955.812 km
Eccentricity
0.00017
Inclination
97.6743°
RAAN
155.085°
Arg. of periapsis
85.1889°
True anomaly
274.93319°
Mean anomaly
274.9531°
Eccentric anomaly
274.94314°
Mean motion
3.74129 °/min
Orbital period
96.22 mins
BSTAR
0.00014534
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-23 04:55:45.206Z | 44.865° NE | 2026-09-23 04:58:45.206Z | 103.623° ESE | 26.296° | 2026-09-23 05:01:45.206Z | 152.716° SSE |
| 5 mins | 2026-09-23 06:31:45.206Z | 328.451° NNW | 2026-09-23 06:33:45.206Z | 289.025° WNW | 23.087° | 2026-09-23 06:36:45.206Z | 240.09° WSW |
| 6 mins | 2026-09-23 17:19:45.206Z | 206.958° SW | 2026-09-23 17:21:45.206Z | 255.146° W | 37.362° | 2026-09-23 17:25:45.206Z | 330.797° NNW |
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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