Showing default

ICEYE-X73, 68496

Orbit data source: Space-Track

ICEYE-X73, 68496 is a Portuguese payload satellite in SSO that was launched on Mon, 30 Mar 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
68496, 2026-067CJ
Orbit
SSO
Country
Flag of PTPT / POR
Related business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
2026-03-30 (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: 11 hours ago

TLE from 11 hours ago
0 ICEYE-X73
1 68496U 26067CJ  26263.10505351  .00001593  00000-0  16036-3 0  9990
2 68496  97.7714 220.0877 0002370  35.8658 324.2720 14.92585966 25881
Epoch: 2026-09-20T02:31Z
TLE epoch observation values (Epoch: 2026-09-20T02:31:16.623Z)
Latitude
-0°
Longitude
-176.73558°
Altitude
591.577 km
Speed
7.565 km/s
True Right ascension
14h 40m 21s
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
06:55:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.545 km
Perigee altitude
585.243 km
Semi-major axis
6,965.031 km
Eccentricity
0.00024
Inclination
97.7714°
RAAN
220.0877°
Arg. of periapsis
35.8658°
True anomaly
324.25614°
Mean anomaly
324.272°
Eccentric anomaly
324.26407°
Mean motion
3.73386 °/min
Orbital period
96.41 mins
BSTAR
0.00016036
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
|