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: 1 day ago
TLE from 1 day ago
0 ICEYE-X2
1 43800U 18099AU 26172.49296225 .00006604 00000-0 32996-3 0 9997
2 43800 97.4353 226.2595 0008514 289.8796 70.1520 15.17766719413470Epoch: 2026-06-21T11:49Z
TLE epoch observation values (Epoch: 2026-06-21T11:49:51.938Z)
Latitude
-0.00002°
Longitude
139.10065°
Altitude
513.69 km
Speed
7.608 km/s
True Right ascension
15h 05m 02s
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
23:19:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
515.426 km
Perigee altitude
503.698 km
Semi-major axis
6,887.699 km
Eccentricity
0.00085
Inclination
97.4353°
RAAN
226.2595°
Arg. of periapsis
289.8796°
True anomaly
70.2438°
Mean anomaly
70.152°
Eccentric anomaly
70.1979°
Mean motion
3.79692 °/min
Orbital period
94.81 mins
BSTAR
0.00032996
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 16:53:25.847Z | 343.952° N | 2026-06-22 16:55:25.847Z | 277.979° WNW | 34.185° | 2026-06-22 16:58:25.847Z | 216.483° SW |
| 6 mins | 2026-06-23 03:31:25.847Z | 157.338° SSE | 2026-06-23 03:34:25.847Z | 25.244° NE | 41.247° | 2026-06-23 03:37:25.847Z | 353.004° N |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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