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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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-X49
1 62384U 24247H 25346.19287046 .00013134 00000-0 79423-3 0 9999
2 62384 44.9980 274.1034 0001527 31.0323 329.0643 15.10671866 53878Epoch: 2025-12-12T04:37Z
TLE epoch observation values (Epoch: 2025-12-12T04:37:44.007Z)
Latitude
-0.00006°
Longitude
123.53196°
Altitude
533.243 km
Speed
7.598 km/s
True Right ascension
18h 16m 24s
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
05:23:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
536.803 km
Perigee altitude
534.692 km
Semi-major axis
6,913.884 km
Eccentricity
0.00015
Inclination
44.998°
RAAN
274.1034°
Arg. of periapsis
31.0323°
True anomaly
329.0553°
Mean anomaly
329.0643°
Eccentric anomaly
329.0598°
Mean motion
3.77537 °/min
Orbital period
95.35 mins
BSTAR
0.00079423
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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 | 2025-12-13 22:05:30.845Z | 218.457° SW | 2025-12-13 22:08:30.845Z | 152.16° SSE | 36.159° | 2025-12-13 22:11:30.845Z | 79.198° E |
| 5 mins | 2025-12-13 23:46:30.845Z | 279.766° WNW | 2025-12-13 23:48:30.845Z | 344.428° N | 38.329° | 2025-12-13 23:51:30.845Z | 58.945° ENE |
| 6 mins | 2025-12-14 01:26:30.845Z | 303.693° NW | 2025-12-14 01:28:30.845Z | 347.827° N | 32.092° | 2025-12-14 01:32:30.845Z | 74.299° E |
| 6 mins | 2025-12-14 03:06:30.845Z | 295.742° NW | 2025-12-14 03:09:30.845Z | 87.773° E | 43.687° | 2025-12-14 03:12:30.845Z | 110.613° ESE |
| 4 mins | 2025-12-14 04:47:30.845Z | 245.952° WSW | 2025-12-14 04:48:30.845Z | 225.022° WSW | 20.886° | 2025-12-14 04:51:30.845Z | 170.806° S |
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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