Showing default

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.

Loading next visibility...
Identifier
62384, 2024-247H
Orbit
LEO
Country
Flag of FIFI / FIN
Related business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
2024-12-21 (8 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 ICEYE-X49
1 62384U 24247H   25240.97781022  .00009269  00000-0  59668-3 0  9994
2 62384  44.9985 112.8640 0003079 150.8827 209.2221 15.08681196 37975
Epoch: 2025-08-28T23:28Z
TLE epoch observation values (Epoch: 2025-08-28T23:28:02.802Z)
Latitude
-0.00003°
Longitude
143.41923°
Altitude
542.086 km
Speed
7.592 km/s
True Right ascension
07h 31m 27s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
16:56:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
543.956 km
Perigee altitude
539.694 km
Semi-major axis
6,919.962 km
Eccentricity
0.00031
Inclination
44.9985°
RAAN
112.864°
Arg. of periapsis
150.8827°
True anomaly
209.20488°
Mean anomaly
209.2221°
Eccentric anomaly
209.21349°
Mean motion
3.7704 °/min
Orbital period
95.48 mins
BSTAR
0.00059668
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|