ICEYE-X2, 43800
Orbit data source: Space-Track
ICEYE-X2, 43800 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Mon, 03 Dec 2018 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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43800 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, 1.6 m
Radar Cross Section
1.837 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 ICEYE-X2
1 43800U 18099AU 25341.31798305 .00010826 00000-0 58374-3 0 9990
2 43800 97.4644 33.6083 0009519 245.8818 114.1419 15.14912237383745Epoch: 2025-12-07T07:37Z
TLE epoch observation values (Epoch: 2025-12-07T07:37:53.735Z)
Latitude
-0.00003°
Longitude
-157.19869°
Altitude
527.019 km
Speed
7.598 km/s
True Right ascension
02h 14m 25s
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
21:28:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
524.785 km
Perigee altitude
511.655 km
Semi-major axis
6,896.357 km
Eccentricity
0.00095
Inclination
97.4644°
RAAN
33.6083°
Arg. of periapsis
245.8818°
True anomaly
114.24139°
Mean anomaly
114.1419°
Eccentric anomaly
114.19165°
Mean motion
3.78978 °/min
Orbital period
94.99 mins
BSTAR
0.00058374
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Other satellites on launch #99 in the year 2018 (2018-12-03 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-X2 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-08 02:48:55.289Z | 103.086° ESE | 2025-12-08 02:50:55.289Z | 63.925° ENE | 18.355° | 2025-12-08 02:52:55.289Z | 28.245° NE |
| 5 mins | 2025-12-08 04:22:55.289Z | 222.072° SW | 2025-12-08 04:24:55.289Z | 270.339° WNW | 24.155° | 2025-12-08 04:27:55.289Z | 322.722° NNW |
| 4 mins | 2025-12-08 15:55:55.289Z | 57.408° ENE | 2025-12-08 15:57:55.289Z | 111.649° ESE | 25.07° | 2025-12-08 15:59:55.289Z | 150.616° SSE |
| 4 mins | 2025-12-08 17:29:55.289Z | 319.789° NNW | 2025-12-08 17:30:55.289Z | 301.234° NW | 16.79° | 2025-12-08 17:33:55.289Z | 248.867° W |
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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