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.
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69011 intel report (Beta)
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Identifier
Orbit
Country
PL / POLRelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Radar Imaging
Bus & Motor
MP42, Unknown motor
Mass
200 kg wet, 200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
0.688 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 EYECORE 1
1 69011U 26100AH 26237.62832329 .00003720 00000-0 17006-3 0 9990
2 69011 97.3953 134.2397 0005659 134.0935 226.0767 15.21156548 17369Epoch: 2026-08-25T15:04Z
TLE epoch observation values (Epoch: 2026-08-25T15:04:47.132Z)
Latitude
-0.00004°
Longitude
-65.84962°
Altitude
508.146 km
Speed
7.608 km/s
True Right ascension
08h 56m 57s
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
19:48:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.207 km
Perigee altitude
495.423 km
Semi-major axis
6,877.452 km
Eccentricity
0.00057
Inclination
97.3953°
RAAN
134.2397°
Arg. of periapsis
134.0935°
True anomaly
226.03002°
Mean anomaly
226.0767°
Eccentric anomaly
226.05336°
Mean motion
3.80541 °/min
Orbital period
94.6 mins
BSTAR
0.00017006
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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.EYECORE 1 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 | 2026-08-26 05:50:43.240Z | 20.017° NNE | 2026-08-26 05:53:43.240Z | 66.058° ENE | 39.235° | 2026-08-26 05:57:43.240Z | 181.315° SSW |
| 4 mins | 2026-08-26 16:29:43.240Z | 110.794° ESE | 2026-08-26 16:31:43.240Z | 67.162° ENE | 21.241° | 2026-08-26 16:33:43.240Z | 26.251° NE |
| 4 mins | 2026-08-26 18:03:43.240Z | 231.141° WSW | 2026-08-26 18:05:43.240Z | 274.536° WNW | 19.068° | 2026-08-26 18:07:43.240Z | 310.595° 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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