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: 20 hours ago
TLE from 20 hours ago
0 ICEYE-X46
1 63258U 25052BA 25287.63560784 .00004478 00000-0 42691-3 0 9999
2 63258 97.7099 178.9725 0001678 86.3832 273.7580 14.93845287 31960Epoch: 2025-10-14T15:15Z
TLE epoch observation values (Epoch: 2025-10-14T15:15:16.517Z)
Latitude
-0.00001°
Longitude
-73.26752°
Altitude
588.929 km
Speed
7.566 km/s
True Right ascension
11h 55m 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
05:48:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.141 km
Perigee altitude
581.805 km
Semi-major axis
6,961.11 km
Eccentricity
0.00017
Inclination
97.7099°
RAAN
178.9725°
Arg. of periapsis
86.3832°
True anomaly
273.73881°
Mean anomaly
273.758°
Eccentric anomaly
273.74841°
Mean motion
3.73702 °/min
Orbital period
96.33 mins
BSTAR
0.00042691
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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 | 2025-10-15 17:07:02.965Z | 184.908° SSW | 2025-10-15 17:09:02.965Z | 245.59° WSW | 41.692° | 2025-10-15 17:13:02.965Z | 340.624° N |
| 4 mins | 2025-10-16 04:50:02.965Z | 66.355° ENE | 2025-10-16 04:51:02.965Z | 84.204° E | 17.959° | 2025-10-16 04:54:02.965Z | 135.518° SSE |
| 5 mins | 2025-10-16 06:25:02.965Z | 335.184° NNW | 2025-10-16 06:27:02.965Z | 288.227° WNW | 27.535° | 2025-10-16 06:30:02.965Z | 231.195° 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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