ICEYE-X14, 51070 (Decayed)
Orbit data source: Space-Track
ICEYE-X14, 51070 was a payload satellite owned by ICEYE US (US) in LEO that was launched on Thu, 13 Jan 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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51070 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
ICEYE US
Mission
Decayed 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 & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 ICEYE-X14
1 51070U 22002CQ 26006.24307145 .14454479 24771-5 43730-3 0 9993
2 51070 97.2904 88.1922 0009282 279.8573 80.1680 16.44421868221897Epoch: 2026-01-06T05:50Z
TLE epoch observation values (Epoch: 2026-01-06T05:50:01.373Z)
Latitude
-0.00011°
Longitude
-105.14219°
Altitude
156.296 km
Speed
7.813 km/s
True Right ascension
05h 52m 46s
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
10:55:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
156.923 km
Perigee altitude
144.803 km
Semi-major axis
6,529 km
Eccentricity
0.00093
Inclination
97.2904°
RAAN
88.1922°
Arg. of periapsis
279.8573°
True anomaly
80.27282°
Mean anomaly
80.168°
Eccentric anomaly
80.22041°
Mean motion
4.11408 °/min
Orbital period
87.5 mins
BSTAR
0.0004373
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Other satellites on launch #2 in the year 2022 (2022-01-13 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-X14 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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