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, 0.6 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 ICEYE-X76
1 68502U 26067CQ 26193.88154102 .00000542 00000-0 59282-4 0 9993
2 68502 97.7640 151.7521 0000718 335.7023 24.4162 14.91747895 15557Epoch: 2026-07-12T21:09Z
TLE epoch observation values (Epoch: 2026-07-12T21:09:25.144Z)
Latitude
0.00002°
Longitude
-96.37671°
Altitude
595.071 km
Speed
7.563 km/s
True Right ascension
10h 07m 00s
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
22:14:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.005 km
Perigee altitude
589.004 km
Semi-major axis
6,967.641 km
Eccentricity
0.00007
Inclination
97.764°
RAAN
151.7521°
Arg. of periapsis
335.7023°
True anomaly
24.4196°
Mean anomaly
24.4162°
Eccentric anomaly
24.4179°
Mean motion
3.73177 °/min
Orbital period
96.47 mins
BSTAR
0.000059282
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-07-13 10:35:51.344Z | 354.301° N | 2026-07-13 10:38:51.344Z | 300.788° NW | 32.707° | 2026-07-13 10:42:51.344Z | 218.952° SW |
| 8 mins | 2026-07-13 21:24:51.344Z | 175.41° S | 2026-07-13 21:28:51.344Z | 247.944° W | 42.605° | 2026-07-13 21:32:51.344Z | 341.648° N |
| 4 mins | 2026-07-14 09:10:51.344Z | 67.697° E | 2026-07-14 09:11:51.344Z | 85.436° E | 17.799° | 2026-07-14 09:14:51.344Z | 135.477° SSE |
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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