ICEYE-X20, 52759
Orbit data source: Space-Track
ICEYE-X20, 52759 is a Finnish payload satellite in SSO that was launched on Wed, 25 May 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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52759 intel report (Beta)
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ICEYE-X20 radio frequencies
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Edit Public Description
Identifier
Orbit
Last TLE update
1 day ago
Origin
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, 1.6 m
Radar Cross Section
1.837 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & history
TLE from 1 day ago
0 ICEYE-X20
1 52759U 22057AD 25232.93337375 .00216636 00000-0 96383-3 0 9994
2 52759 97.5973 34.8515 0003105 305.6890 54.4090 15.83743359181578Epoch: 2025-08-20T22:24Z
TLE epoch observation values (Epoch: 2025-08-20T22:24:03.492Z)
Latitude
0.00005°
Longitude
89.33286°
Altitude
321.826 km
Speed
7.716 km/s
True Right ascension
02h 19m 24s
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
13:23:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
318.834 km
Perigee altitude
314.677 km
Semi-major axis
6,694.892 km
Eccentricity
0.00031
Inclination
97.5973°
RAAN
34.8515°
Arg. of periapsis
305.689°
True anomaly
54.43794°
Mean anomaly
54.409°
Eccentric anomaly
54.42347°
Mean motion
3.96212 °/min
Orbital period
90.86 mins
BSTAR
0.00096383
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Other satellites on launch #57 in the year 2022 (2022-05-25 UTC)
ICEYE-X20 Visibility
Observer location: undefined°, undefined°
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. |
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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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Authenticating...
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