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: 8 hours ago
TLE from 8 hours ago
0 ICEYE-X71
1 68494U 26067CG 26260.16668981 .00053930 00000-0 44386-2 0 9990
2 68494 97.7719 217.2764 0004195 81.1591 172.4883 14.98870019 5797Epoch: 2026-09-17T04:00Z
TLE epoch observation values (Epoch: 2026-09-17T04:00:01.999Z)
Latitude
-72.08079°
Longitude
-43.6605°
Altitude
599.93 km
Speed
7.557 km/s
True Right ascension
00h 49m 49s
True Declination
-71° 58' 39"
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
05:13:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.31 km
Perigee altitude
564.483 km
Semi-major axis
6,945.533 km
Eccentricity
0.00042
Inclination
97.7719°
RAAN
217.2764°
Arg. of periapsis
81.1591°
True anomaly
172.49458°
Mean anomaly
172.4883°
Eccentric anomaly
172.49144°
Mean motion
3.7496 °/min
Orbital period
96.01 mins
BSTAR
0.0044386
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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 | 2026-09-17 20:37:48.418Z | 130.681° SE | 2026-09-17 20:40:48.418Z | 77.666° E | 30.911° | 2026-09-17 20:43:48.418Z | 14.944° NNE |
| 4 mins | 2026-09-17 22:14:48.418Z | 240.205° WSW | 2026-09-17 22:15:48.418Z | 258.49° W | 18.565° | 2026-09-17 22:18:48.418Z | 308.944° NW |
| 6 mins | 2026-09-18 09:53:48.418Z | 27.739° NE | 2026-09-18 09:55:48.418Z | 73.767° E | 55.362° | 2026-09-18 09:59:48.418Z | 179.519° S |
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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