ICEYE-X47, 62389
Orbit data source: Space-Track
ICEYE-X47, 62389 is a payload satellite owned by ICEYE (FI) in LEO that was launched on Sat, 21 Dec 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62389 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
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 ICEYE-X47
1 62389U 24247N 26221.60869204 .00002420 00000-0 14637-3 0 9997
2 62389 44.9964 71.5906 0002240 216.7146 143.3578 15.13660504 90279Epoch: 2026-08-09T14:36Z
TLE epoch observation values (Epoch: 2026-08-09T14:36:30.992Z)
Latitude
-0.00004°
Longitude
-105.64181°
Altitude
526.287 km
Speed
7.601 km/s
True Right ascension
04h 46m 21s
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
21:50:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.195 km
Perigee altitude
525.102 km
Semi-major axis
6,904.785 km
Eccentricity
0.00022
Inclination
44.9964°
RAAN
71.5906°
Arg. of periapsis
216.7146°
True anomaly
143.37312°
Mean anomaly
143.3578°
Eccentric anomaly
143.36546°
Mean motion
3.78284 °/min
Orbital period
95.17 mins
BSTAR
0.00014637
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Other satellites on launch #247 in the year 2024 (2024-12-21 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-X47 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 | 2026-08-10 16:07:22.045Z | 180.581° SSW | 2026-08-10 16:09:22.045Z | 148.138° SSE | 17.625° | 2026-08-10 16:12:22.045Z | 97.066° ESE |
| 6 mins | 2026-08-10 17:46:22.045Z | 243.697° WSW | 2026-08-10 17:49:22.045Z | 79.139° E | 44.357° | 2026-08-10 17:52:22.045Z | 67.008° ENE |
| 6 mins | 2026-08-10 19:26:22.045Z | 288.65° WNW | 2026-08-10 19:29:22.045Z | 4.519° NNE | 32.966° | 2026-08-10 19:32:22.045Z | 62.173° ENE |
| 5 mins | 2026-08-10 21:07:22.045Z | 310.521° NW | 2026-08-10 21:09:22.045Z | 15.248° NNE | 36.569° | 2026-08-10 21:12:22.045Z | 84.041° E |
| 6 mins | 2026-08-10 22:46:22.045Z | 283.321° WNW | 2026-08-10 22:49:22.045Z | 193.369° SSW | 39.174° | 2026-08-10 22:52:22.045Z | 134.08° SE |
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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