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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Edit Public Description
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, 0.7 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 ICEYE-X46
1 63258U 25052BA 25334.64881235 .00005061 00000-0 47510-3 0 9994
2 63258 97.7087 225.1289 0001951 76.5395 283.6043 14.94396791 38981Epoch: 2025-11-30T15:34Z
TLE epoch observation values (Epoch: 2025-11-30T15:34:17.387Z)
Latitude
0.00004°
Longitude
-78.20319°
Altitude
586.973 km
Speed
7.567 km/s
True Right ascension
15h 00m 30s
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
01:15:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.617 km
Perigee altitude
579.901 km
Semi-major axis
6,959.396 km
Eccentricity
0.0002
Inclination
97.7087°
RAAN
225.1289°
Arg. of periapsis
76.5395°
True anomaly
283.58257°
Mean anomaly
283.6043°
Eccentric anomaly
283.59343°
Mean motion
3.7384 °/min
Orbital period
96.3 mins
BSTAR
0.0004751
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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 | 2025-12-01 05:00:34.702Z | 43.988° NE | 2025-12-01 05:03:34.702Z | 100.988° ESE | 23.835° | 2025-12-01 05:06:34.702Z | 151.64° SSE |
| 5 mins | 2025-12-01 06:36:34.702Z | 331.098° NNW | 2025-12-01 06:38:34.702Z | 293.056° NW | 21.519° | 2025-12-01 06:41:34.702Z | 241.587° WSW |
| 5 mins | 2025-12-01 17:25:34.702Z | 211.541° SW | 2025-12-01 17:27:34.702Z | 265.649° W | 30.954° | 2025-12-01 17:30:34.702Z | 325.681° 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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