ICEYE-X76, 68502
Orbit data source: Space-Track
ICEYE-X76, 68502 is a payload satellite owned by ICEYE (PL) 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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68502 intel report (Beta)
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Identifier
Orbit
Country
PL / POLRelated 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: 19 hours ago
TLE from 19 hours ago
0 ICEYE-X76
1 68502U 26067CQ 26236.13900616 .00000678 00000-0 72740-4 0 9992
2 68502 97.7684 193.3886 0003175 119.8956 240.2579 14.91815408 21853Epoch: 2026-08-24T03:20Z
TLE epoch observation values (Epoch: 2026-08-24T03:20:10.132Z)
Latitude
0.00004°
Longitude
170.92138°
Altitude
596.415 km
Speed
7.561 km/s
True Right ascension
12h 53m 33s
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
13:53:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.506 km
Perigee altitude
587.082 km
Semi-major axis
6,967.431 km
Eccentricity
0.00032
Inclination
97.7684°
RAAN
193.3886°
Arg. of periapsis
119.8956°
True anomaly
240.22632°
Mean anomaly
240.2579°
Eccentric anomaly
240.24211°
Mean motion
3.73194 °/min
Orbital period
96.46 mins
BSTAR
0.00007274
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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-X76 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 | 2026-08-25 10:29:54.656Z | 352.962° N | 2026-08-25 10:32:54.656Z | 263.22° W | 35.831° | 2026-08-25 10:35:54.656Z | 214.201° SW |
| 6 mins | 2026-08-25 21:19:54.656Z | 172.324° S | 2026-08-25 21:21:54.656Z | 206.054° SW | 44.135° | 2026-08-25 21:25:54.656Z | 345.271° 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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