ICEYE-X14, 51070
Orbit data source: Space-Track
ICEYE-X14, 51070 is a payload satellite owned by ICEYE US (US) in SSO 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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ICEYE US
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 & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 ICEYE-X14
1 51070U 22002CQ 25291.19057878 .00159220 00000-0 19226-2 0 9994
2 51070 97.3290 3.5160 0003850 204.7266 155.3807 15.60199360209272Epoch: 2025-10-18T04:34Z
TLE epoch observation values (Epoch: 2025-10-18T04:34:26.006Z)
Latitude
-0.00004°
Longitude
-92.0175°
Altitude
392.596 km
Speed
7.673 km/s
True Right ascension
00h 14m 03s
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
04:23:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
386.593 km
Perigee altitude
381.386 km
Semi-major axis
6,762.127 km
Eccentricity
0.00039
Inclination
97.329°
RAAN
3.516°
Arg. of periapsis
204.7266°
True anomaly
155.39907°
Mean anomaly
155.3807°
Eccentric anomaly
155.38989°
Mean motion
3.90318 °/min
Orbital period
92.23 mins
BSTAR
0.0019226
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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 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 | 2025-10-18 17:26:41.115Z | 30.842° NE | 2025-10-18 17:29:41.115Z | 119.916° SE | 29.375° | 2025-10-18 17:31:41.115Z | 165.269° S |
| 4 mins | 2025-10-19 05:20:41.115Z | 204.009° SW | 2025-10-19 05:21:41.115Z | 235.847° WSW | 31.228° | 2025-10-19 05:24:41.115Z | 330.907° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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