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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Edit Public Description
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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ICEYE-X5
1 44389U 19038C 25287.96185267 .00026868 00000-0 73477-3 0 9998
2 44389 97.9071 316.2668 0010528 61.8654 298.3652 15.37294130345070Epoch: 2025-10-14T23:05Z
TLE epoch observation values (Epoch: 2025-10-14T23:05:04.070Z)
Latitude
0°
Longitude
-53.74292°
Altitude
453.801 km
Speed
7.642 km/s
True Right ascension
21h 05m 04s
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
08:41:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.27 km
Perigee altitude
443.89 km
Semi-major axis
6,829.217 km
Eccentricity
0.00105
Inclination
97.9071°
RAAN
316.2668°
Arg. of periapsis
61.8654°
True anomaly
298.25898°
Mean anomaly
298.3652°
Eccentric anomaly
298.31209°
Mean motion
3.8458 °/min
Orbital period
93.61 mins
BSTAR
0.00073477
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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 | 2025-10-15 15:15:55.204Z | 353.796° N | 2025-10-15 15:17:55.204Z | 310.104° NW | 32.932° | 2025-10-15 15:20:55.204Z | 218.179° SW |
| 5 mins | 2025-10-16 01:46:55.204Z | 145.747° SSE | 2025-10-16 01:48:55.204Z | 89.31° E | 37.933° | 2025-10-16 01:51:55.204Z | 359.461° N |
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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