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: 4 hours ago
TLE from 4 hours ago
0 ICEYE-X76
1 68502U 26067CQ 26295.83269118 .00001171 00000-0 12134-3 0 9998
2 68502 97.7795 252.2704 0001420 357.4897 2.6315 14.91920948 30758Epoch: 2026-10-22T19:59Z
TLE epoch observation values (Epoch: 2026-10-22T19:59:04.517Z)
Latitude
0.00001°
Longitude
-78.76035°
Altitude
593.999 km
Speed
7.563 km/s
True Right ascension
16h 49m 04s
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
19:09:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.955 km
Perigee altitude
587.977 km
Semi-major axis
6,967.103 km
Eccentricity
0.00014
Inclination
97.7795°
RAAN
252.2704°
Arg. of periapsis
357.4897°
True anomaly
2.63225°
Mean anomaly
2.6315°
Eccentric anomaly
2.63187°
Mean motion
3.7322 °/min
Orbital period
96.46 mins
BSTAR
0.00012134
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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 | 2026-10-23 09:26:06.450Z | 37.007° NE | 2026-10-23 09:29:06.450Z | 85.245° E | 28.694° | 2026-10-23 09:33:06.450Z | 157.356° SSE |
| 5 mins | 2026-10-23 11:03:06.450Z | 325.863° NNW | 2026-10-23 11:05:06.450Z | 287.489° WNW | 21.814° | 2026-10-23 11:08:06.450Z | 241.507° WSW |
| 4 mins | 2026-10-23 20:18:06.450Z | 92.537° ESE | 2026-10-23 20:19:06.450Z | 74.378° E | 19.393° | 2026-10-23 20:22:06.450Z | 24.763° NE |
| 6 mins | 2026-10-23 21:52:06.450Z | 206.607° SW | 2026-10-23 21:55:06.450Z | 272.728° WNW | 32.491° | 2026-10-23 21:58:06.450Z | 324.595° NNW |
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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