ICEYE-X73, 68496
Orbit data source: Space-Track
ICEYE-X73, 68496 is a payload satellite owned by ICEYE (PT) 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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68496 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, 0.6 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-X73
1 68496U 26067CJ 26171.38551196 .00001812 00000-0 18325-3 0 9993
2 68496 97.7608 129.6374 0000939 16.3079 343.8170 14.92236289 12208Epoch: 2026-06-20T09:15Z
TLE epoch observation values (Epoch: 2026-06-20T09:15:08.233Z)
Latitude
-0.00002°
Longitude
82.25221°
Altitude
593.378 km
Speed
7.564 km/s
True Right ascension
08h 38m 32s
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
13:50:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.637 km
Perigee altitude
587.328 km
Semi-major axis
6,966.12 km
Eccentricity
0.00009
Inclination
97.7608°
RAAN
129.6374°
Arg. of periapsis
16.3079°
True anomaly
343.814°
Mean anomaly
343.817°
Eccentric anomaly
343.8155°
Mean motion
3.73299 °/min
Orbital period
96.44 mins
BSTAR
0.00018325
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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-X73 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 | 2026-06-22 10:05:32.822Z | 13.161° NNE | 2026-06-22 10:09:32.822Z | 174.207° S | 44.589° | 2026-06-22 10:12:32.822Z | 192.019° SSW |
| 6 mins | 2026-06-22 20:56:32.822Z | 140.766° SSE | 2026-06-22 20:58:32.822Z | 91.485° ESE | 37.742° | 2026-06-22 21:02:32.822Z | 359.049° N |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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