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: 19 hours ago
TLE from 19 hours ago
0 ICEYE-X4
1 44390U 19038D 25322.54481612 .00014014 00000-0 58271-3 0 9992
2 44390 97.8976 338.6661 0014016 325.9819 34.0517 15.23823423349661Epoch: 2025-11-18T13:04Z
TLE epoch observation values (Epoch: 2025-11-18T13:04:32.112Z)
Latitude
-0.00004°
Longitude
84.70293°
Altitude
489.423 km
Speed
7.625 km/s
True Right ascension
22h 34m 39s
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
04:34:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.931 km
Perigee altitude
481.675 km
Semi-major axis
6,869.44 km
Eccentricity
0.0014
Inclination
97.8976°
RAAN
338.6661°
Arg. of periapsis
325.9819°
True anomaly
34.14176°
Mean anomaly
34.0517°
Eccentric anomaly
34.09672°
Mean motion
3.81207 °/min
Orbital period
94.44 mins
BSTAR
0.00058271
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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 | 2025-11-19 13:17:58.343Z | 56.209° ENE | 2025-11-19 13:19:58.343Z | 95.001° ESE | 18.375° | 2025-11-19 13:21:58.343Z | 133.919° SE |
| 4 mins | 2025-11-19 14:51:58.343Z | 326.648° NNW | 2025-11-19 14:53:58.343Z | 277.503° WNW | 22.111° | 2025-11-19 14:55:58.343Z | 240.129° WSW |
| 5 mins | 2025-11-20 01:27:58.343Z | 186.696° SSW | 2025-11-20 01:29:58.343Z | 275.974° WNW | 40.705° | 2025-11-20 01:32:58.343Z | 338.843° N |
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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