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ICEYE X78, 68995

AKA "ICEYE-X78" on Space-Track | Orbit data source: Space-Track

ICEYE X78, 68995 is a Polish payload satellite in SSO that was launched on Sun, 03 May 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.

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Identifier
68995, 2026-100R
Orbit
SSO
Country
Flag of PLPL / POL
Related business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
2026-05-03 (5 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: 8 hours ago

TLE from 8 hours ago
0 ICEYE X78
1 68995U 26100R   26266.13585634  .00000681  00000-0  72841-4 0  9994
2 68995  97.7229 161.7107 0003114 133.5035 226.6443 14.91906576 21308
Epoch: 2026-09-23T03:15Z
TLE epoch observation values (Epoch: 2026-09-23T03:15:37.987Z)
Latitude
-0.00006°
Longitude
110.81111°
Altitude
596.525 km
Speed
7.561 km/s
True Right ascension
10h 46m 50s
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
04:07:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.178 km
Perigee altitude
586.839 km
Semi-major axis
6,967.145 km
Eccentricity
0.00031
Inclination
97.7229°
RAAN
161.7107°
Arg. of periapsis
133.5035°
True anomaly
226.61836°
Mean anomaly
226.6443°
Eccentric anomaly
226.63133°
Mean motion
3.73217 °/min
Orbital period
96.46 mins
BSTAR
0.000072841
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