ICEYE-X5, 44389
Orbit data source: Space-Track
ICEYE-X5, 44389 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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44389 intel report (Beta)
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Identifier
Orbit
Country
FI / FINRelated business
Manufacturer
ICEYE
Mission
Non-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: 4 hours ago
TLE from 4 hours ago
0 ICEYE-X5
1 44389U 19038C 26306.19937399 .00077507 00000-0 62446-3 0 9997
2 44389 97.8513 16.0790 0004544 113.6548 246.5190 15.70663107404507Epoch: 2026-11-02T04:47Z
TLE epoch observation values (Epoch: 2026-11-02T04:47:05.912Z)
Latitude
-0.00009°
Longitude
-97.17544°
Altitude
361.367 km
Speed
7.692 km/s
True Right ascension
01h 04m 18s
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
04:53:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
356.978 km
Perigee altitude
350.86 km
Semi-major axis
6,732.056 km
Eccentricity
0.00045
Inclination
97.8513°
RAAN
16.079°
Arg. of periapsis
113.6548°
True anomaly
246.47125°
Mean anomaly
246.519°
Eccentric anomaly
246.49513°
Mean motion
3.92936 °/min
Orbital period
91.62 mins
BSTAR
0.00062446
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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-X5 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 | 2026-11-02 17:34:09.817Z | 20.687° NNE | 2026-11-02 17:36:09.817Z | 52.025° ENE | 49.341° | 2026-11-02 17:39:09.817Z | 182.442° SSW |
| 4 mins | 2026-11-03 05:23:09.817Z | 214.015° SW | 2026-11-03 05:25:09.817Z | 274.072° WNW | 23.941° | 2026-11-03 05:27:09.817Z | 319.302° NNW |
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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