Showing default

ICEYE-X72, 68504

Orbit data source: Space-Track

ICEYE-X72, 68504 is a payload satellite owned by ICEYE (FI) 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
68504, 2026-067CS
Orbit
SSO
Country
Flag of FIFI / FIN
Related business
Manufacturer
ICEYE
Mission
Operational spacecraft
Bus & Motor
ICEYE, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
2026-03-30 (1 month ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 ICEYE-X72
1 68504U 26067CS  26127.59986604  .00001397  00000-0  14386-3 0  9994
2 68504  97.7603  86.5024 0003417 100.4605 259.6999 14.91841918  5676
Epoch: 2026-05-07T14:23Z
TLE epoch observation values (Epoch: 2026-05-07T14:23:48.425Z)
Latitude
-0.00004°
Longitude
5.10695°
Altitude
595.661 km
Speed
7.562 km/s
True Right ascension
05h 46m 00s
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
05:06:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.592 km
Perigee altitude
586.831 km
Semi-major axis
6,967.348 km
Eccentricity
0.00034
Inclination
97.7603°
RAAN
86.5024°
Arg. of periapsis
100.4605°
True anomaly
259.66138°
Mean anomaly
259.6999°
Eccentric anomaly
259.68064°
Mean motion
3.732 °/min
Orbital period
96.46 mins
BSTAR
0.00014386
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
|