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: 14 hours ago
TLE from 14 hours ago
0 ICEYE-X2
1 43800U 18099AU 26235.63775317 .00009065 00000-0 44262-3 0 9990
2 43800 97.4305 288.3015 0011721 71.3918 288.8588 15.18432720423057Epoch: 2026-08-23T15:18Z
TLE epoch observation values (Epoch: 2026-08-23T15:18:21.873Z)
Latitude
-0.00006°
Longitude
86.77943°
Altitude
511.062 km
Speed
7.61 km/s
True Right ascension
19h 13m 12s
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
20:02:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
515.616 km
Perigee altitude
499.475 km
Semi-major axis
6,885.683 km
Eccentricity
0.00117
Inclination
97.4305°
RAAN
288.3015°
Arg. of periapsis
71.3918°
True anomaly
288.73164°
Mean anomaly
288.8588°
Eccentric anomaly
288.79522°
Mean motion
3.79859 °/min
Orbital period
94.77 mins
BSTAR
0.00044262
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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 | 2026-08-24 15:36:56.951Z | 57.115° ENE | 2026-08-24 15:38:56.951Z | 95.665° ESE | 17.903° | 2026-08-24 15:40:56.951Z | 133.25° SE |
| 4 mins | 2026-08-24 17:10:56.951Z | 331.846° NNW | 2026-08-24 17:12:56.951Z | 285.565° WNW | 23.15° | 2026-08-24 17:14:56.951Z | 242.939° WSW |
| 6 mins | 2026-08-25 03:48:56.951Z | 180.567° SSW | 2026-08-25 03:50:56.951Z | 217.761° SW | 40.131° | 2026-08-25 03:54:56.951Z | 341.594° N |
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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