ICEYE-X18, 52749 (Decayed)
Orbit data source: Space-Track
ICEYE-X18, 52749 was a Brazilian payload satellite in LEO 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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52749 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 ICEYE-X18
1 52749U 22057T 25070.75847188 .15490060 26594-5 38355-3 0 9998
2 52749 97.5453 211.7976 0011682 275.8963 84.1006 16.45158447155727Epoch: 2025-03-11T18:12Z
TLE epoch observation values (Epoch: 2025-03-11T18:12:11.970Z)
Latitude
-0.00012°
Longitude
129.09092°
Altitude
154.594 km
Speed
7.814 km/s
True Right ascension
14h 07m 11s
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
13:49:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
156.549 km
Perigee altitude
141.299 km
Semi-major axis
6,527.061 km
Eccentricity
0.00117
Inclination
97.5453°
RAAN
211.7976°
Arg. of periapsis
275.8963°
True anomaly
84.23378°
Mean anomaly
84.1006°
Eccentric anomaly
84.16719°
Mean motion
4.11592 °/min
Orbital period
87.47 mins
BSTAR
0.00038355
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Other satellites on launch #57 in the year 2022 (2022-05-25 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-X18 Visibility
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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. |
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| This satellite is decayed. |
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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