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: 9 hours ago
TLE from 9 hours ago
0 ICEYE X78
1 68995U 26100R 26168.67917807 .00001790 00000-0 18311-3 0 9998
2 68995 97.7365 66.1267 0003812 109.1925 250.9706 14.91770064 6773Epoch: 2026-06-17T16:18Z
TLE epoch observation values (Epoch: 2026-06-17T16:18:00.985Z)
Latitude
-0.00007°
Longitude
-84.31079°
Altitude
596.326 km
Speed
7.561 km/s
True Right ascension
04h 24m 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
12:13:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.09 km
Perigee altitude
586.778 km
Semi-major axis
6,967.571 km
Eccentricity
0.00038
Inclination
97.7365°
RAAN
66.1267°
Arg. of periapsis
109.1925°
True anomaly
250.92931°
Mean anomaly
250.9706°
Eccentric anomaly
250.94996°
Mean motion
3.73182 °/min
Orbital period
96.47 mins
BSTAR
0.00018311
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-18 05:44:39.330Z | 23.62° NE | 2026-06-18 05:48:39.330Z | 118.236° SE | 38.006° | 2026-06-18 05:51:39.330Z | 174.629° S |
| 6 mins | 2026-06-18 16:35:39.330Z | 124.995° SE | 2026-06-18 16:38:39.330Z | 56.273° ENE | 27.777° | 2026-06-18 16:41:39.330Z | 8.869° NNE |
| 4 mins | 2026-06-18 18:12:39.330Z | 245.04° WSW | 2026-06-18 18:13:39.330Z | 263.501° W | 17.812° | 2026-06-18 18:16:39.330Z | 310.884° NW |
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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