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 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: 20 hours ago
TLE from 20 hours ago
0 ICEYE-X71
1 68494U 26067CG 26263.45688879 .00006405 00000-0 52733-3 0 9994
2 68494 97.7735 220.5576 0002853 74.1855 285.9683 14.99434745 25958Epoch: 2026-09-20T10:57Z
TLE epoch observation values (Epoch: 2026-09-20T10:57:55.191Z)
Latitude
0.00005°
Longitude
56.72683°
Altitude
571.149 km
Speed
7.576 km/s
True Right ascension
14h 42m 13s
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
00:08:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
567.632 km
Perigee altitude
563.67 km
Semi-major axis
6,943.788 km
Eccentricity
0.00029
Inclination
97.7735°
RAAN
220.5576°
Arg. of periapsis
74.1855°
True anomaly
285.93687°
Mean anomaly
285.9683°
Eccentric anomaly
285.95258°
Mean motion
3.75101 °/min
Orbital period
95.97 mins
BSTAR
0.00052733
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-21 09:56:38.626Z | 18.184° NNE | 2026-09-21 10:00:38.626Z | 103.548° ESE | 66.368° | 2026-09-21 10:03:38.626Z | 181.693° SSW |
| 6 mins | 2026-09-21 20:44:38.626Z | 128.626° SE | 2026-09-21 20:46:38.626Z | 87.105° E | 35.04° | 2026-09-21 20:50:38.626Z | 6.011° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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