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: 10 hours ago
TLE from 10 hours ago
0 ICEYE-X4
1 44390U 19038D 26199.85960904 .00005998 00000-0 20942-3 0 9990
2 44390 97.8744 234.6477 0013248 185.0655 175.0452 15.29927976386640Epoch: 2026-07-18T20:37Z
TLE epoch observation values (Epoch: 2026-07-18T20:37:50.221Z)
Latitude
-0.00002°
Longitude
-11.47786°
Altitude
488.166 km
Speed
7.616 km/s
True Right ascension
15h 38m 35s
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
19:53:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.077 km
Perigee altitude
463.924 km
Semi-major axis
6,851.138 km
Eccentricity
0.00132
Inclination
97.8744°
RAAN
234.6477°
Arg. of periapsis
185.0655°
True anomaly
175.05829°
Mean anomaly
175.0452°
Eccentric anomaly
175.05175°
Mean motion
3.82736 °/min
Orbital period
94.06 mins
BSTAR
0.00020942
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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 | 2026-07-19 14:28:18.972Z | 49.227° ENE | 2026-07-19 14:30:18.972Z | 84.974° E | 17.83° | 2026-07-19 14:32:18.972Z | 128.978° SE |
| 4 mins | 2026-07-19 16:02:18.972Z | 326.79° NNW | 2026-07-19 16:04:18.972Z | 279.397° WNW | 20.022° | 2026-07-19 16:06:18.972Z | 241.921° WSW |
| 5 mins | 2026-07-20 02:35:18.972Z | 181.446° SSW | 2026-07-20 02:37:18.972Z | 222.802° SW | 39.677° | 2026-07-20 02:40:18.972Z | 336.996° NNW |
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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