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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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, 2.4 m
Radar Cross Section
1.837 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X2
1 43800U 18099AU 26296.18162326 .00014081 00000-0 66599-3 0 9998
2 43800 97.4211 347.7856 0009136 207.3699 152.7056 15.19451984432244Epoch: 2026-10-23T04:21Z
TLE epoch observation values (Epoch: 2026-10-23T04:21:32.249Z)
Latitude
0°
Longitude
-109.20462°
Altitude
516.178 km
Speed
7.602 km/s
True Right ascension
23h 11m 08s
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
05:14:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.751 km
Perigee altitude
498.175 km
Semi-major axis
6,882.6 km
Eccentricity
0.00091
Inclination
97.4211°
RAAN
347.7856°
Arg. of periapsis
207.3699°
True anomaly
152.75356°
Mean anomaly
152.7056°
Eccentric anomaly
152.72958°
Mean motion
3.80114 °/min
Orbital period
94.71 mins
BSTAR
0.00066599
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-23 15:59:40.524Z | 33.993° NE | 2026-10-23 16:02:40.524Z | 108.33° ESE | 36.776° | 2026-10-23 16:05:40.524Z | 165.988° S |
| 5 mins | 2026-10-24 04:12:40.524Z | 218.956° SW | 2026-10-24 04:14:40.524Z | 275.747° WNW | 30.633° | 2026-10-24 04:17:40.524Z | 327.163° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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