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: 18 hours ago
TLE from 18 hours ago
0 ICEYE-X49
1 62384U 24247H 25300.61652276 .00006641 00000-0 41938-3 0 9992
2 62384 44.9974 156.3515 0002532 157.0550 203.0440 15.09778702 46989Epoch: 2025-10-27T14:47Z
TLE epoch observation values (Epoch: 2025-10-27T14:47:47.566Z)
Latitude
0.00001°
Longitude
-101.81249°
Altitude
538.485 km
Speed
7.594 km/s
True Right ascension
10h 25m 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
04:01:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.224 km
Perigee altitude
536.722 km
Semi-major axis
6,916.61 km
Eccentricity
0.00025
Inclination
44.9974°
RAAN
156.3515°
Arg. of periapsis
157.055°
True anomaly
203.03265°
Mean anomaly
203.044°
Eccentric anomaly
203.03832°
Mean motion
3.77314 °/min
Orbital period
95.41 mins
BSTAR
0.00041938
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-28 16:22:51.915Z | 165.735° S | 2025-10-28 16:24:51.915Z | 132.29° SE | 15.088° | 2025-10-28 16:26:51.915Z | 102.093° ESE |
| 6 mins | 2025-10-28 18:01:51.915Z | 234.875° WSW | 2025-10-28 18:03:51.915Z | 183.836° SSW | 43.76° | 2025-10-28 18:07:51.915Z | 68.764° E |
| 6 mins | 2025-10-28 19:41:51.915Z | 288.502° WNW | 2025-10-28 19:43:51.915Z | 334.145° NNW | 33.778° | 2025-10-28 19:47:51.915Z | 63.16° ENE |
| 6 mins | 2025-10-28 21:21:51.915Z | 301.931° NW | 2025-10-28 21:24:51.915Z | 16.746° NNE | 35.349° | 2025-10-28 21:27:51.915Z | 80.597° E |
| 6 mins | 2025-10-28 23:02:51.915Z | 282.908° WNW | 2025-10-28 23:04:51.915Z | 209.725° SW | 42.449° | 2025-10-28 23:08:51.915Z | 126.215° SE |
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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