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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 spacecraft
Bus & Motor
ICEYE, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
2026-05-03 (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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 ICEYE X82
1 68996U 26100S   26168.62621950  .00001558  00000-0  16189-3 0  9998
2 68996  97.7360  66.0389 0005196 130.3262 229.8411 14.91304494  6767
Epoch: 2026-06-17T15:01Z
TLE epoch observation values (Epoch: 2026-06-17T15:01:45.364Z)
Latitude
-0.00006°
Longitude
-65.28131°
Altitude
599.247 km
Speed
7.559 km/s
True Right ascension
04h 24m 09s
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
12:52:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.507 km
Perigee altitude
587.264 km
Semi-major axis
6,969.022 km
Eccentricity
0.00052
Inclination
97.736°
RAAN
66.0389°
Arg. of periapsis
130.3262°
True anomaly
229.79561°
Mean anomaly
229.8411°
Eccentric anomaly
229.81835°
Mean motion
3.73066 °/min
Orbital period
96.5 mins
BSTAR
0.00016189
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