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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ICEYE-X4 radio frequencies
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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: 22 hours ago
TLE from 22 hours ago
0 ICEYE-X4
1 44390U 19038D 25261.30291983 .00009266 00000-0 41002-3 0 9995
2 44390 97.9037 274.2781 0016357 165.0345 195.1377 15.21794986340343Epoch: 2025-09-18T07:16Z
TLE epoch observation values (Epoch: 2025-09-18T07:16:12.273Z)
Latitude
-0.00002°
Longitude
167.76051°
Altitude
514.369 km
Speed
7.601 km/s
True Right ascension
18h 17m 06s
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
21:40:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.658 km
Perigee altitude
486.165 km
Semi-major axis
6,875.549 km
Eccentricity
0.00164
Inclination
97.9037°
RAAN
274.2781°
Arg. of periapsis
165.0345°
True anomaly
195.08885°
Mean anomaly
195.1377°
Eccentric anomaly
195.11326°
Mean motion
3.80699 °/min
Orbital period
94.56 mins
BSTAR
0.00041002
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-19 13:48:48.071Z | 14.572° NNE | 2025-09-19 13:51:48.071Z | 58.823° ENE | 44.568° | 2025-09-19 13:54:48.071Z | 190.48° SSW |
| 5 mins | 2025-09-20 00:26:48.071Z | 126.473° SE | 2025-09-20 00:28:48.071Z | 80.558° E | 28.137° | 2025-09-20 00:31:48.071Z | 11.597° NNE |
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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