ICEYE-X49, 62384
Orbit data source: Space-Track
ICEYE-X49, 62384 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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62384 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: 2 days ago
TLE from 2 days ago
0 ICEYE-X49
1 62384U 24247H 26219.98416075 .00001545 00000-0 98990-4 0 9996
2 62384 44.9984 80.6979 0001367 271.3688 88.7033 15.13492843 90024Epoch: 2026-08-07T23:37Z
TLE epoch observation values (Epoch: 2026-08-07T23:37:11.488Z)
Latitude
-0.00003°
Longitude
129.89798°
Altitude
525.535 km
Speed
7.602 km/s
True Right ascension
05h 22m 47s
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
22:54:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.102 km
Perigee altitude
526.214 km
Semi-major axis
6,905.295 km
Eccentricity
0.00014
Inclination
44.9984°
RAAN
80.6979°
Arg. of periapsis
271.3688°
True anomaly
88.71896°
Mean anomaly
88.7033°
Eccentric anomaly
88.71113°
Mean motion
3.78242 °/min
Orbital period
95.18 mins
BSTAR
0.00009899
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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-X49 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 | 2026-08-10 16:45:11.557Z | 206.812° SW | 2026-08-10 16:48:11.557Z | 147.4° SSE | 29.191° | 2026-08-10 16:51:11.557Z | 84.788° E |
| 6 mins | 2026-08-10 18:25:11.557Z | 264.663° W | 2026-08-10 18:28:11.557Z | 8.641° NNE | 40.648° | 2026-08-10 18:31:11.557Z | 61.767° ENE |
| 5 mins | 2026-08-10 20:06:11.557Z | 308.062° NW | 2026-08-10 20:08:11.557Z | 7.253° NNE | 31.939° | 2026-08-10 20:11:11.557Z | 67.137° ENE |
| 5 mins | 2026-08-10 21:46:11.557Z | 304.054° NW | 2026-08-10 21:48:11.557Z | 22.624° NE | 42.374° | 2026-08-10 21:51:11.557Z | 99.765° ESE |
| 5 mins | 2026-08-10 23:26:11.557Z | 255.698° W | 2026-08-10 23:28:11.557Z | 201.681° SSW | 26.583° | 2026-08-10 23:31:11.557Z | 153.575° 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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