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 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: 18 hours ago
TLE from 18 hours ago
0 ICEYE X78
1 68995U 26100R 26220.66163092 .00000584 00000-0 63325-4 0 9991
2 68995 97.7297 117.1281 0001729 354.3313 5.7886 14.91848628 14529Epoch: 2026-08-08T15:52Z
TLE epoch observation values (Epoch: 2026-08-08T15:52:44.911Z)
Latitude
-0.00003°
Longitude
-78.22879°
Altitude
594.015 km
Speed
7.564 km/s
True Right ascension
07h 48m 30s
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
23:34:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.394 km
Perigee altitude
587.984 km
Semi-major axis
6,967.326 km
Eccentricity
0.00017
Inclination
97.7297°
RAAN
117.1281°
Arg. of periapsis
354.3313°
True anomaly
5.7906°
Mean anomaly
5.7886°
Eccentric anomaly
5.7896°
Mean motion
3.73202 °/min
Orbital period
96.46 mins
BSTAR
0.000063325
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-09 16:10:52.172Z | 105.966° ESE | 2026-08-09 16:12:52.172Z | 74.666° E | 17.425° | 2026-08-09 16:15:52.172Z | 25.83° NE |
| 6 mins | 2026-08-09 17:45:52.172Z | 204.498° SW | 2026-08-09 17:48:52.172Z | 272.228° WNW | 29.318° | 2026-08-09 17:51:52.172Z | 325.562° NNW |
| 5 mins | 2026-08-10 05:29:52.172Z | 47.253° ENE | 2026-08-10 05:31:52.172Z | 95.526° ESE | 29.605° | 2026-08-10 05:34:52.172Z | 157.662° S |
| 4 mins | 2026-08-10 07:05:52.172Z | 317.587° NNW | 2026-08-10 07:06:52.172Z | 299.926° NW | 17.535° | 2026-08-10 07:09:52.172Z | 251.336° W |
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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