ICEYE-X53, 64584
Orbit data source: Space-Track
ICEYE-X53, 64584 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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64584 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, 0.8 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-X53
1 64584U 25135BJ 26036.28703207 .00009208 00000-0 72815-3 0 9994
2 64584 97.7473 153.5703 0001168 86.6807 273.4551 15.00864535 34293Epoch: 2026-02-05T06:53Z
TLE epoch observation values (Epoch: 2026-02-05T06:53:19.570Z)
Latitude
0.00002°
Longitude
-85.20267°
Altitude
567.235 km
Speed
7.577 km/s
True Right ascension
10h 14m 16s
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
14:07:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.046 km
Perigee altitude
560.425 km
Semi-major axis
6,939.372 km
Eccentricity
0.00012
Inclination
97.7473°
RAAN
153.5703°
Arg. of periapsis
86.6807°
True anomaly
273.44174°
Mean anomaly
273.4551°
Eccentric anomaly
273.44842°
Mean motion
3.75459 °/min
Orbital period
95.88 mins
BSTAR
0.00072815
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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-X53 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-05 20:15:09.402Z | 24.658° NE | 2026-02-05 20:19:09.402Z | 120.821° SE | 36.414° | 2026-02-05 20:22:09.402Z | 173.782° S |
| 4 mins | 2026-02-06 07:03:09.402Z | 107.269° ESE | 2026-02-06 07:05:09.402Z | 58.35° ENE | 24.452° | 2026-02-06 07:07:09.402Z | 20.601° NNE |
| 4 mins | 2026-02-06 08:38:09.402Z | 234.866° WSW | 2026-02-06 08:40:09.402Z | 275.116° WNW | 19.117° | 2026-02-06 08:42:09.402Z | 308.66° NW |
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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