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 25348.77292549 .00008120 00000-0 49495-3 0 9999
2 62389 44.9965 260.3262 0000806 350.4450 9.6411 15.10822743 54264Epoch: 2025-12-14T18:33Z
TLE epoch observation values (Epoch: 2025-12-14T18:33:00.762Z)
Latitude
-0.00002°
Longitude
-101.60803°
Altitude
533.139 km
Speed
7.598 km/s
True Right ascension
17h 21m 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
17:09:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.845 km
Perigee altitude
534.73 km
Semi-major axis
6,913.425 km
Eccentricity
0.00008
Inclination
44.9965°
RAAN
260.3262°
Arg. of periapsis
350.445°
True anomaly
9.64265°
Mean anomaly
9.6411°
Eccentric anomaly
9.64187°
Mean motion
3.77575 °/min
Orbital period
95.35 mins
BSTAR
0.00049495
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-15 21:45:09.399Z | 235.541° WSW | 2025-12-15 21:48:09.399Z | 135.308° SSE | 43.649° | 2025-12-15 21:51:09.399Z | 70.215° E |
| 5 mins | 2025-12-15 23:26:09.399Z | 292.255° WNW | 2025-12-15 23:28:09.399Z | 351.029° N | 34.61° | 2025-12-15 23:31:09.399Z | 59.339° ENE |
| 6 mins | 2025-12-16 01:06:09.399Z | 305.753° NW | 2025-12-16 01:08:09.399Z | 351.019° N | 34.317° | 2025-12-16 01:12:09.399Z | 82.509° E |
| 6 mins | 2025-12-16 02:46:09.399Z | 286.425° WNW | 2025-12-16 02:48:09.399Z | 253.341° W | 40.933° | 2025-12-16 02:52:09.399Z | 126.006° SE |
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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