Showing default

ICEYE-X64, 67373

Orbit data source: Space-Track

ICEYE-X64, 67373 is a Finnish payload satellite in SSO that was launched on Sun, 11 Jan 2026 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
67373, 2026-004L
Orbit
SSO
Country
Flag of FIFI / FIN
Related business
Manufacturer
ICEYE
Mission
Operational Defense Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
2026-01-11 (6 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, 2.4 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-X64
1 67373U 26004L   26205.44570114  .00001050  00000-0  12034-3 0  9998
2 67373  97.8034 203.4220 0006626  28.2996 331.8579 14.88003154 28839
Epoch: 2026-07-24T10:41Z
TLE epoch observation values (Epoch: 2026-07-24T10:41:48.578Z)
Latitude
-0.00006°
Longitude
100.79737°
Altitude
603.131 km
Speed
7.56 km/s
True Right ascension
13h 33m 41s
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
11:11:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.826 km
Perigee altitude
596.577 km
Semi-major axis
6,979.338 km
Eccentricity
0.00066
Inclination
97.8034°
RAAN
203.422°
Arg. of periapsis
28.2996°
True anomaly
331.82206°
Mean anomaly
331.8579°
Eccentric anomaly
331.83998°
Mean motion
3.72239 °/min
Orbital period
96.71 mins
BSTAR
0.00012034
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
|