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: 8 hours ago
TLE from 8 hours ago
0 ICEYE-X49
1 62384U 24247H 26094.20574040 .00012445 00000-0 71886-3 0 9994
2 62384 44.9995 32.1543 0001213 306.3557 53.7208 15.12371355 70970Epoch: 2026-04-04T04:56Z
TLE epoch observation values (Epoch: 2026-04-04T04:56:15.970Z)
Latitude
-0.00003°
Longitude
125.55888°
Altitude
528.473 km
Speed
7.601 km/s
True Right ascension
02h 08m 37s
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
19:11:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.407 km
Perigee altitude
529.731 km
Semi-major axis
6,908.706 km
Eccentricity
0.00012
Inclination
44.9995°
RAAN
32.1543°
Arg. of periapsis
306.3557°
True anomaly
53.73201°
Mean anomaly
53.7208°
Eccentric anomaly
53.7264°
Mean motion
3.77962 °/min
Orbital period
95.25 mins
BSTAR
0.00071886
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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 | 2026-04-04 22:33:25.555Z | 205.824° SW | 2026-04-04 22:36:25.555Z | 150.811° SSE | 28.015° | 2026-04-04 22:39:25.555Z | 86.849° E |
| 6 mins | 2026-04-05 00:13:25.555Z | 262.171° W | 2026-04-05 00:16:25.555Z | 355.07° N | 41.843° | 2026-04-05 00:19:25.555Z | 61.469° ENE |
| 5 mins | 2026-04-05 01:54:25.555Z | 303.979° NW | 2026-04-05 01:56:25.555Z | 356.829° N | 32.108° | 2026-04-05 01:59:25.555Z | 64.626° ENE |
| 6 mins | 2026-04-05 03:34:25.555Z | 302.567° NW | 2026-04-05 03:36:25.555Z | 351.741° N | 41.201° | 2026-04-05 03:40:25.555Z | 100.292° ESE |
| 5 mins | 2026-04-05 05:14:25.555Z | 263.71° W | 2026-04-05 05:16:25.555Z | 214.328° SW | 28.37° | 2026-04-05 05:19:25.555Z | 155.089° 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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