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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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, 0.8 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ICEYE-X47
1 62389U 24247N 26036.19338019 .00016465 00000-0 96183-3 0 9990
2 62389 44.9982 341.2504 0001178 286.3301 73.7446 15.11770157 62199Epoch: 2026-02-05T04:38Z
TLE epoch observation values (Epoch: 2026-02-05T04:38:28.048Z)
Latitude
-0.00004°
Longitude
136.28437°
Altitude
530.572 km
Speed
7.599 km/s
True Right ascension
22h 45m 00s
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
06:43:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
533.214 km
Perigee altitude
531.586 km
Semi-major axis
6,910.537 km
Eccentricity
0.00012
Inclination
44.9982°
RAAN
341.2504°
Arg. of periapsis
286.3301°
True anomaly
73.75756°
Mean anomaly
73.7446°
Eccentric anomaly
73.75108°
Mean motion
3.77812 °/min
Orbital period
95.29 mins
BSTAR
0.00096183
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-06 04:54:14.015Z | 287.422° WNW | 2026-02-06 04:57:14.015Z | 212.35° SW | 42.183° | 2026-02-06 05:01:14.015Z | 126.757° SE |
| 6 mins | 2026-02-06 23:42:14.015Z | 245.292° WSW | 2026-02-06 23:44:14.015Z | 245.02° WSW | 42.883° | 2026-02-06 23:48:14.015Z | 66.528° ENE |
| 6 mins | 2026-02-07 01:22:14.015Z | 290.569° WNW | 2026-02-07 01:25:14.015Z | 10.007° NNE | 32.568° | 2026-02-07 01:28:14.015Z | 63.224° ENE |
| 5 mins | 2026-02-07 03:03:14.015Z | 310.38° NW | 2026-02-07 03:05:14.015Z | 15.962° NNE | 37.072° | 2026-02-07 03:08:14.015Z | 85.074° E |
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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