DECAYED
Showing default

KEPLER-12 (BOBA), 47446 (Decayed)

Orbit data source: Space-Track

KEPLER-12 (BOBA), 47446 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
47446, 2021-006AK
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, 0.5 m
Radar Cross Section
0.196 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 months ago

TLE from 11 months ago
0 KEPLER-12 (BOBA)
1 47446U 21006AK  24284.45247648  .16290543  25048-5  62844-3 0  9995
2 47446  97.2833 346.8369 0010266 263.3369  96.6764 16.43111867206560
Epoch: 2024-10-10T10:51Z
TLE epoch observation values (Epoch: 2024-10-10T10:51:33.967Z)
Latitude
-0.00006°
Longitude
164.40856°
Altitude
161.584 km
Speed
7.809 km/s
True Right ascension
23h 07m 20s
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
23:56:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
161.042 km
Perigee altitude
147.63 km
Semi-major axis
6,532.473 km
Eccentricity
0.00103
Inclination
97.2833°
RAAN
346.8369°
Arg. of periapsis
263.3369°
True anomaly
96.79322°
Mean anomaly
96.6764°
Eccentric anomaly
96.73481°
Mean motion
4.1108 °/min
Orbital period
87.57 mins
BSTAR
0.00062844
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|