ICEYE-X4, 44390
Orbit data source: Space-Track
ICEYE-X4, 44390 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Fri, 05 Jul 2019 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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44390 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: 4 hours ago
TLE from 4 hours ago
0 ICEYE-X4
1 44390U 19038D 26306.20061670 .00009645 00000-0 31438-3 0 9996
2 44390 97.8618 347.4094 0012659 172.4312 187.7122 15.31976290402912Epoch: 2026-11-02T04:48Z
TLE epoch observation values (Epoch: 2026-11-02T04:48:53.282Z)
Latitude
-0.00002°
Longitude
-126.29365°
Altitude
481.602 km
Speed
7.62 km/s
True Right ascension
23h 09m 38s
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
04:53:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.552 km
Perigee altitude
458.221 km
Semi-major axis
6,845.024 km
Eccentricity
0.00127
Inclination
97.8618°
RAAN
347.4094°
Arg. of periapsis
172.4312°
True anomaly
187.69276°
Mean anomaly
187.7122°
Eccentric anomaly
187.70248°
Mean motion
3.83249 °/min
Orbital period
93.93 mins
BSTAR
0.00031438
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Other satellites on launch #38 in the year 2019 (2019-07-05 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-X4 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 | 2026-11-02 16:21:42.663Z | 333.995° NNW | 2026-11-02 16:23:42.663Z | 274.511° WNW | 29.664° | 2026-11-02 16:25:42.663Z | 231.718° WSW |
| 6 mins | 2026-11-03 02:53:42.663Z | 164.189° S | 2026-11-03 02:55:42.663Z | 156.091° SSE | 63.996° | 2026-11-03 02:59:42.663Z | 348.729° 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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