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ICEYE X82, 68996

AKA "ICEYE-X82" on Space-Track | Orbit data source: Space-Track

ICEYE X82, 68996 is a payload satellite owned by ICEYE (PT) 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
68996, 2026-100S
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)
2026-05-03 (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 X82
1 68996U 26100S   26266.17242438  .00001338  00000-0  13860-3 0  9996
2 68996  97.7222 161.6514 0004197 160.5432 199.5948 14.91660292 21306
Epoch: 2026-09-23T04:08Z
TLE epoch observation values (Epoch: 2026-09-23T04:08:17.466Z)
Latitude
Longitude
97.55126°
Altitude
598.558 km
Speed
7.559 km/s
True Right ascension
10h 46m 36s
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
05:22:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.7 km
Perigee altitude
586.851 km
Semi-major axis
6,967.913 km
Eccentricity
0.00042
Inclination
97.7222°
RAAN
161.6514°
Arg. of periapsis
160.5432°
True anomaly
199.57868°
Mean anomaly
199.5948°
Eccentric anomaly
199.58674°
Mean motion
3.73155 °/min
Orbital period
96.47 mins
BSTAR
0.0001386
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