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: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X46
1 63258U 25052BA 26121.17682248 .00003599 00000-0 32990-3 0 9990
2 63258 97.6942 13.9631 0001541 92.5424 267.5974 14.95518404 61629Epoch: 2026-05-01T04:14Z
TLE epoch observation values (Epoch: 2026-05-01T04:14:37.462Z)
Latitude
0.00005°
Longitude
91.19417°
Altitude
583.858 km
Speed
7.568 km/s
True Right ascension
00h 55m 51s
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
18:10:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.847 km
Perigee altitude
576.703 km
Semi-major axis
6,955.912 km
Eccentricity
0.00015
Inclination
97.6942°
RAAN
13.9631°
Arg. of periapsis
92.5424°
True anomaly
267.57976°
Mean anomaly
267.5974°
Eccentric anomaly
267.58858°
Mean motion
3.74121 °/min
Orbital period
96.23 mins
BSTAR
0.0003299
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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 | 2026-05-01 17:13:44.938Z | 196.782° SSW | 2026-05-01 17:15:44.938Z | 250.251° W | 36.4° | 2026-05-01 17:19:44.938Z | 335.261° NNW |
| 5 mins | 2026-05-02 04:55:44.938Z | 58.335° ENE | 2026-05-02 04:57:44.938Z | 99.785° ESE | 21.955° | 2026-05-02 05:00:44.938Z | 148.804° SSE |
| 5 mins | 2026-05-02 06:30:44.938Z | 332.401° NNW | 2026-05-02 06:32:44.938Z | 292.283° WNW | 23.08° | 2026-05-02 06:35:44.938Z | 238.767° WSW |
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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