ICEYE X78, 68995
AKA "ICEYE-X78" on Space-Track | Orbit data source: Space-Track
ICEYE X78, 68995 is a Polish payload satellite in SSO that was launched on Sun, 03 May 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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68995 intel report (Beta)
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Identifier
Orbit
Country
PL / POLRelated 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, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ICEYE X78
1 68995U 26100R 26175.05138437 .00001889 00000-0 19292-3 0 9990
2 68995 97.7363 72.3796 0004133 96.6645 263.5044 14.91779032 7728Epoch: 2026-06-24T01:13Z
TLE epoch observation values (Epoch: 2026-06-24T01:13:59.609Z)
Latitude
-0.00006°
Longitude
141.66709°
Altitude
595.758 km
Speed
7.562 km/s
True Right ascension
04h 49m 31s
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
16:59:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.286 km
Perigee altitude
586.526 km
Semi-major axis
6,967.543 km
Eccentricity
0.00041
Inclination
97.7363°
RAAN
72.3796°
Arg. of periapsis
96.6645°
True anomaly
263.45735°
Mean anomaly
263.5044°
Eccentric anomaly
263.48087°
Mean motion
3.73185 °/min
Orbital period
96.47 mins
BSTAR
0.00019292
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Other satellites on launch #100 in the year 2026 (2026-05-03 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 X78 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 | 2026-06-25 06:46:15.167Z | 346.179° N | 2026-06-25 06:49:15.167Z | 293.513° NW | 25.692° | 2026-06-25 06:52:15.167Z | 235.811° WSW |
| 5 mins | 2026-06-25 17:37:15.167Z | 201.74° SSW | 2026-06-25 17:39:15.167Z | 260.525° W | 35.512° | 2026-06-25 17:42:15.167Z | 329.374° NNW |
| 5 mins | 2026-06-26 05:20:15.167Z | 49.086° ENE | 2026-06-26 05:22:15.167Z | 86.818° E | 23.846° | 2026-06-26 05:25:15.167Z | 146.107° 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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