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: 17 hours ago
TLE from 17 hours ago
0 ICEYE-X2
1 43800U 18099AU 25292.29069527 .00016025 00000-0 88588-3 0 9996
2 43800 97.4732 345.4970 0012373 63.5750 296.6750 15.13901313376326Epoch: 2025-10-19T06:58Z
TLE epoch observation values (Epoch: 2025-10-19T06:58:36.071Z)
Latitude
0°
Longitude
-147.16277°
Altitude
523.57 km
Speed
7.604 km/s
True Right ascension
23h 01m 59s
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
18:30:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.83 km
Perigee altitude
512.756 km
Semi-major axis
6,899.43 km
Eccentricity
0.00124
Inclination
97.4732°
RAAN
345.497°
Arg. of periapsis
63.575°
True anomaly
296.54822°
Mean anomaly
296.675°
Eccentric anomaly
296.61162°
Mean motion
3.78724 °/min
Orbital period
95.06 mins
BSTAR
0.00088588
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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 | 2025-10-20 03:43:16.028Z | 168.205° S | 2025-10-20 03:46:16.028Z | 181.765° SSW | 44.3° | 2025-10-20 03:49:16.028Z | 346.82° N |
| 5 mins | 2025-10-20 16:52:16.028Z | 346.777° N | 2025-10-20 16:54:16.028Z | 264.829° W | 36.971° | 2025-10-20 16:57:16.028Z | 210.911° SW |
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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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 ascending order |
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