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: 1 day ago
TLE from 1 day ago
0 ICEYE-X71
1 68494U 26067CG 26217.00002315 -.00078313 00000-0 -76975-2 0 9991
2 68494 97.7634 174.5179 0001373 181.5813 83.6323 14.92587696 5674Epoch: 2026-08-05T00:00Z
TLE epoch observation values (Epoch: 2026-08-05T00:00:02.000Z)
Latitude
-80.95157°
Longitude
-17.41944°
Altitude
617.973 km
Speed
7.549 km/s
True Right ascension
19h 44m 35s
True Declination
-80° 53' 49"
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
20:29:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.845 km
Perigee altitude
585.932 km
Semi-major axis
6,965.025 km
Eccentricity
0.00014
Inclination
97.7634°
RAAN
174.5179°
Arg. of periapsis
181.5813°
True anomaly
83.64794°
Mean anomaly
83.6323°
Eccentric anomaly
83.64012°
Mean motion
3.73387 °/min
Orbital period
96.41 mins
BSTAR
-0.0076975
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-06 09:11:37.394Z | 51.323° ENE | 2026-08-06 09:14:37.394Z | 102.528° ESE | 18.525° | 2026-08-06 09:16:37.394Z | 135.04° SSE |
| 5 mins | 2026-08-06 10:47:37.394Z | 337.073° NNW | 2026-08-06 10:49:37.394Z | 293.413° NW | 27.154° | 2026-08-06 10:52:37.394Z | 233.519° WSW |
| 6 mins | 2026-08-06 21:36:37.394Z | 191.093° SSW | 2026-08-06 21:39:37.394Z | 274.342° WNW | 36.928° | 2026-08-06 21:42:37.394Z | 332.996° 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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