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: 15 hours ago
TLE from 15 hours ago
0 ICEYE-X47
1 62389U 24247N 26023.43866381 .00011792 00000-0 69989-3 0 9993
2 62389 44.9952 49.1946 0002000 278.1963 81.8687 15.11431683 60269Epoch: 2026-01-23T10:31Z
TLE epoch observation values (Epoch: 2026-01-23T10:31:40.553Z)
Latitude
0°
Longitude
128.49817°
Altitude
531.636 km
Speed
7.599 km/s
True Right ascension
03h 16m 46s
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
03:06:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.814 km
Perigee altitude
532.049 km
Semi-major axis
6,911.569 km
Eccentricity
0.0002
Inclination
44.9952°
RAAN
49.1946°
Arg. of periapsis
278.1963°
True anomaly
81.89139°
Mean anomaly
81.8687°
Eccentric anomaly
81.88004°
Mean motion
3.77727 °/min
Orbital period
95.31 mins
BSTAR
0.00069989
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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 | 2026-01-24 04:08:51.265Z | 200.956° SSW | 2026-01-24 04:11:51.265Z | 152.575° SSE | 24.201° | 2026-01-24 04:14:51.265Z | 91.595° ESE |
| 7 mins | 2026-01-24 05:48:51.265Z | 255.9° W | 2026-01-24 05:51:51.265Z | 337.915° N | 43.659° | 2026-01-24 05:55:51.265Z | 64.595° ENE |
| 6 mins | 2026-01-24 07:29:51.265Z | 299.382° NW | 2026-01-24 07:31:51.265Z | 347.533° N | 32.118° | 2026-01-24 07:35:51.265Z | 68.039° E |
| 6 mins | 2026-01-24 09:09:51.265Z | 302.598° NW | 2026-01-24 09:12:51.265Z | 45.54° ENE | 38.926° | 2026-01-24 09:15:51.265Z | 94.705° ESE |
| 6 mins | 2026-01-24 10:49:51.265Z | 272.677° WNW | 2026-01-24 10:51:51.265Z | 228.993° WSW | 31.636° | 2026-01-24 10:55:51.265Z | 145.039° SSE |
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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