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 Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
2026-03-30 (4 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: 19 hours ago

TLE from 19 hours ago
0 ICEYE-X72
1 68504U 26067CS  26217.41399403  .00002343  00000-0  20125-3 0  9990
2 68504  97.7636 175.2669 0002597 153.8839 206.2515 14.98422590 19082
Epoch: 2026-08-05T09:56Z
TLE epoch observation values (Epoch: 2026-08-05T09:56:09.084Z)
Latitude
0.00001°
Longitude
72.26031°
Altitude
576.439 km
Speed
7.572 km/s
True Right ascension
11h 41m 04s
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
18:58:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.584 km
Perigee altitude
566.976 km
Semi-major axis
6,946.917 km
Eccentricity
0.00026
Inclination
97.7636°
RAAN
175.2669°
Arg. of periapsis
153.8839°
True anomaly
206.23834°
Mean anomaly
206.2515°
Eccentric anomaly
206.24492°
Mean motion
3.74848 °/min
Orbital period
96.04 mins
BSTAR
0.00020125
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
|