DECAYED
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KEPLER-11 (DANEEL), 47503 (Decayed)

Orbit data source: Space-Track

KEPLER-11 (DANEEL), 47503 was a payload satellite owned by Kepler Comms (CA) in LEO that was launched on Sun, 24 Jan 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.

Not visible in the next 10 days
Identifier
47503, 2021-006CU
Orbit
Decayed
Country
Flag of CACA
Related business
Manufacturer
KEPLER/UTIAS
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
15 kg wet, 15 kg dry
Launch date (UTC)
2021-01-24 (5 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.196 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 7 months ago

TLE from 7 months ago
0 KEPLER-11 (DANEEL)
1 47503U 21006CU  25082.92103752  .02816806  23868-5  92607-3 0  9994
2 47503  97.2577 153.0744 0006876 249.3158 110.7397 16.25945445232012
Epoch: 2025-03-23T22:06Z
TLE epoch observation values (Epoch: 2025-03-23T22:06:17.641Z)
Latitude
-0.00009°
Longitude
-0.14392°
Altitude
208.301 km
Speed
7.78 km/s
True Right ascension
10h 12m 17s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
21:29:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
204.802 km
Perigee altitude
195.755 km
Semi-major axis
6,578.415 km
Eccentricity
0.00069
Inclination
97.2577°
RAAN
153.0744°
Arg. of periapsis
249.3158°
True anomaly
110.81336°
Mean anomaly
110.7397°
Eccentric anomaly
110.77653°
Mean motion
4.06782 °/min
Orbital period
88.5 mins
BSTAR
0.00092607
Loading maneuver chart data...
Computing Atmospheric mass density...

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