ICEYE-X56, 64574
Orbit data source: Space-Track
ICEYE-X56, 64574 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Mon, 23 Jun 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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64574 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 ICEYE-X56
1 64574U 25135AY 26120.19074296 .00003826 00000-0 35225-3 0 9990
2 64574 97.7681 235.5520 0003378 121.7105 238.4445 14.95324802 46756Epoch: 2026-04-30T04:34Z
TLE epoch observation values (Epoch: 2026-04-30T04:34:40.191Z)
Latitude
-0.00007°
Longitude
-51.25635°
Altitude
585.642 km
Speed
7.567 km/s
True Right ascension
15h 42m 12s
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
16:38:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.729 km
Perigee altitude
576.029 km
Semi-major axis
6,956.516 km
Eccentricity
0.00034
Inclination
97.7681°
RAAN
235.552°
Arg. of periapsis
121.7105°
True anomaly
238.41152°
Mean anomaly
238.4445°
Eccentric anomaly
238.42801°
Mean motion
3.74072 °/min
Orbital period
96.24 mins
BSTAR
0.00035225
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-X56 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-30 19:36:46.400Z | 47.957° ENE | 2026-04-30 19:39:46.400Z | 96.121° ESE | 18.273° | 2026-04-30 19:41:46.400Z | 130.848° SE |
| 5 mins | 2026-04-30 21:12:46.400Z | 339.182° N | 2026-04-30 21:14:46.400Z | 297.389° NW | 26.972° | 2026-04-30 21:17:46.400Z | 234.285° WSW |
| 6 mins | 2026-05-01 08:00:46.400Z | 190.167° SSW | 2026-05-01 08:03:46.400Z | 283.288° WNW | 37.183° | 2026-05-01 08:06:46.400Z | 334.95° 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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