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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68996 intel report (Beta)
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Identifier
Orbit
Country
PT / PORRelated business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ICEYE X82
1 68996U 26100S 26220.95778541 .00000858 00000-0 91230-4 0 9995
2 68996 97.7291 117.3471 0003885 356.7246 3.3947 14.91520742 14563Epoch: 2026-08-08T22:59Z
TLE epoch observation values (Epoch: 2026-08-08T22:59:12.659Z)
Latitude
0.00002°
Longitude
175.08268°
Altitude
593.531 km
Speed
7.565 km/s
True Right ascension
07h 49m 23s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
22:29:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.918 km
Perigee altitude
587.504 km
Semi-major axis
6,968.348 km
Eccentricity
0.00039
Inclination
97.7291°
RAAN
117.3471°
Arg. of periapsis
356.7246°
True anomaly
3.39734°
Mean anomaly
3.3947°
Eccentric anomaly
3.39602°
Mean motion
3.7312 °/min
Orbital period
96.48 mins
BSTAR
0.00009123
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Other satellites on launch #100 in the year 2026 (2026-05-03 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ICEYE X82 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-09 16:49:40.691Z | 145.623° SSE | 2026-08-09 16:52:40.691Z | 87.33° E | 37.156° | 2026-08-09 16:56:40.691Z | 359.636° N |
| 6 mins | 2026-08-10 06:09:40.691Z | 6.348° NNE | 2026-08-10 06:11:40.691Z | 336.402° NNW | 43.004° | 2026-08-10 06:15:40.691Z | 199.198° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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