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 spacecraft
Bus & Motor
ICEYE, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 ICEYE X82
1 68996U 26100S 26175.20166422 .00002207 00000-0 22690-3 0 9994
2 68996 97.7356 72.4868 0005573 113.8564 246.3239 14.91329932 7740Epoch: 2026-06-24T04:50Z
TLE epoch observation values (Epoch: 2026-06-24T04:50:23.788Z)
Latitude
-0.00004°
Longitude
87.52542°
Altitude
598.392 km
Speed
7.56 km/s
True Right ascension
04h 49m 56s
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
06:05:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.69 km
Perigee altitude
586.922 km
Semi-major axis
6,968.943 km
Eccentricity
0.00056
Inclination
97.7356°
RAAN
72.4868°
Arg. of periapsis
113.8564°
True anomaly
246.26543°
Mean anomaly
246.3239°
Eccentric anomaly
246.29466°
Mean motion
3.73072 °/min
Orbital period
96.5 mins
BSTAR
0.0002269
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-25 05:34:17.864Z | 33.542° NE | 2026-06-25 05:37:17.864Z | 95.751° ESE | 32.266° | 2026-06-25 05:40:17.864Z | 161.972° S |
| 5 mins | 2026-06-25 16:25:17.864Z | 112.523° SE | 2026-06-25 16:27:17.864Z | 73.961° E | 23.234° | 2026-06-25 16:30:17.864Z | 19.009° NNE |
| 5 mins | 2026-06-25 18:01:17.864Z | 229.29° WSW | 2026-06-25 18:03:17.864Z | 271.545° WNW | 22.283° | 2026-06-25 18:06:17.864Z | 319.024° NNW |
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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