Showing default

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.

Loading next visibility...
Identifier
69011, 2026-100AH
Orbit
SSO
Country
Flag of PLPL / POL
Related business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
Bus & Motor
MP42, Unknown motor
Mass
200 kg wet, 200 kg dry
Launch date (UTC)
2026-05-03 (3 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
1.955 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 EYECORE 1
1 69011U 26100AH  26201.70871216  .00002570  00000-0  11938-3 0  9998
2 69011  97.4003  98.9588 0002630 281.9744  78.1197 15.20893721 11907
Epoch: 2026-07-20T17:00Z
TLE epoch observation values (Epoch: 2026-07-20T17:00:32.730Z)
Latitude
-0.00001°
Longitude
-94.66645°
Altitude
505.863 km
Speed
7.611 km/s
True Right ascension
06h 35m 50s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
05:15:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.917 km
Perigee altitude
498.299 km
Semi-major axis
6,878.245 km
Eccentricity
0.00026
Inclination
97.4003°
RAAN
98.9588°
Arg. of periapsis
281.9744°
True anomaly
78.14919°
Mean anomaly
78.1197°
Eccentric anomaly
78.13445°
Mean motion
3.80476 °/min
Orbital period
94.62 mins
BSTAR
0.00011938
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...

Documentation

Showing up to 5 results
|