ICEYE-X71, 68494
Orbit data source: Space-Track
ICEYE-X71, 68494 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Mon, 30 Mar 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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68494 intel report (Beta)
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Identifier
Orbit
Country
FI / FINRelated 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, 0.7 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 ICEYE-X71
1 68494U 26067CG 26171.34857552 .00002071 00000-0 21147-3 0 9996
2 68494 97.7608 129.5350 0003142 47.5700 312.5784 14.91678262 12197Epoch: 2026-06-20T08:21Z
TLE epoch observation values (Epoch: 2026-06-20T08:21:56.924Z)
Latitude
-0.00006°
Longitude
95.48334°
Altitude
594.262 km
Speed
7.564 km/s
True Right ascension
08h 38m 08s
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
09:12:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.911 km
Perigee altitude
587.532 km
Semi-major axis
6,967.858 km
Eccentricity
0.00031
Inclination
97.7608°
RAAN
129.535°
Arg. of periapsis
47.57°
True anomaly
312.55188°
Mean anomaly
312.5784°
Eccentric anomaly
312.56514°
Mean motion
3.73159 °/min
Orbital period
96.47 mins
BSTAR
0.00021147
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Other satellites on launch #67 in the year 2026 (2026-03-30 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-X71 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 | 2026-06-22 09:14:36.915Z | 45.448° ENE | 2026-06-22 09:17:36.915Z | 94.243° ESE | 20.314° | 2026-06-22 09:20:36.915Z | 143.517° SSE |
| 5 mins | 2026-06-22 10:51:36.915Z | 326.641° NNW | 2026-06-22 10:53:36.915Z | 278.471° WNW | 25.142° | 2026-06-22 10:56:36.915Z | 231.476° WSW |
| 6 mins | 2026-06-22 21:40:36.915Z | 197.203° SSW | 2026-06-22 21:42:36.915Z | 239.864° WSW | 34.06° | 2026-06-22 21:46:36.915Z | 332.161° 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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