EYECORE 1, 69011
AKA "EYCORE-1" on Space-Track | Orbit data source: Space-Track
EYECORE 1, 69011 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.
Focus sentinelFocus sentinel
Request partner network tasking
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
69011 intel report (Beta)
Focus sentinelFocus sentinel
Edit Public Description
Focus sentinelFocus sentinel
Edit Sat Name
Focus sentinelFocus sentinel
Create New Watchlist
Identifier
Orbit
Country
PL / POLRelated business
Manufacturer
NanoAvionics
Mission
Operational spacecraft
Bus & Motor
MP42, Unknown motor
Mass
200 kg wet, 200 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: 14 hours ago
TLE from 14 hours ago
0 EYECORE 1
1 69011U 26100AH 26175.19271919 .00004646 00000-0 21451-3 0 9992
2 69011 97.4046 72.9088 0005192 31.3813 328.7731 15.20686137 7871Epoch: 2026-06-24T04:37Z
TLE epoch observation values (Epoch: 2026-06-24T04:37:30.938Z)
Latitude
-0.00004°
Longitude
91.17644°
Altitude
503.805 km
Speed
7.614 km/s
True Right ascension
04h 51m 38s
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
06:07:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.306 km
Perigee altitude
497.163 km
Semi-major axis
6,878.872 km
Eccentricity
0.00052
Inclination
97.4046°
RAAN
72.9088°
Arg. of periapsis
31.3813°
True anomaly
328.74224°
Mean anomaly
328.7731°
Eccentric anomaly
328.75767°
Mean motion
3.80424 °/min
Orbital period
94.63 mins
BSTAR
0.00021451
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #100 in the year 2026 (2026-05-03 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.EYECORE 1 Visibility forecast
Loading observer location...
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 | 2026-06-25 06:28:19.317Z | 343.011° N | 2026-06-25 06:30:19.317Z | 270.509° WNW | 34.168° | 2026-06-25 06:33:19.317Z | 214.635° SW |
| 5 mins | 2026-06-25 17:05:19.317Z | 152.95° SSE | 2026-06-25 17:07:19.317Z | 100.245° ESE | 41.673° | 2026-06-25 17:10:19.317Z | 356.5° N |
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 |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
|---|