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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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: 8 hours ago
TLE from 8 hours ago
0 ICEYE-X4
1 44390U 19038D 25303.30026208 .00015687 00000-0 66410-3 0 9992
2 44390 97.9009 318.4180 0016221 33.0692 327.1554 15.23155638346735Epoch: 2025-10-30T07:12Z
TLE epoch observation values (Epoch: 2025-10-30T07:12:22.643Z)
Latitude
-0.00006°
Longitude
171.46264°
Altitude
490.044 km
Speed
7.625 km/s
True Right ascension
21h 13m 40s
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
10:54:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.459 km
Perigee altitude
482.167 km
Semi-major axis
6,871.45 km
Eccentricity
0.00162
Inclination
97.9009°
RAAN
318.418°
Arg. of periapsis
33.0692°
True anomaly
327.05441°
Mean anomaly
327.1554°
Eccentric anomaly
327.10492°
Mean motion
3.8104 °/min
Orbital period
94.48 mins
BSTAR
0.0006641
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-31 00:41:18.337Z | 134.255° SE | 2025-10-31 00:44:18.337Z | 55.725° ENE | 29.457° | 2025-10-31 00:46:18.337Z | 12.157° NNE |
| 5 mins | 2025-10-31 13:44:18.337Z | 32.512° NE | 2025-10-31 13:46:18.337Z | 86.065° E | 36.339° | 2025-10-31 13:49:18.337Z | 171.85° S |
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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