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KEPLER-16 (ASTRAEUS), 51057

Orbit data source: Space-Track

KEPLER-16 (ASTRAEUS), 51057 is a payload satellite owned by Kepler Comms (CA) in SSO that was launched on Thu, 13 Jan 2022 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
51057, 2022-002CB
Orbit
SSO
Country
Flag of CACA
Related business
Manufacturer
KEPLER/UTIAS
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
15 kg wet, 15 kg dry
Launch date (UTC)
2022-01-13 (4 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: 1 day ago

TLE from 1 day ago
0 KEPLER-16 (ASTRAEUS)
1 51057U 22002CB  25256.75742454  .00462792  96562-4  83577-3 0  9997
2 51057  97.3012 343.7107 0005720 167.5015 192.6407 16.01561007204985
Epoch: 2025-09-13T18:10Z
TLE epoch observation values (Epoch: 2025-09-13T18:10:41.48Z)
Latitude
-0.00003°
Longitude
78.05167°
Altitude
277.01 km
Speed
7.739 km/s
True Right ascension
22h 54m 50s
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
21:42:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
270.75 km
Perigee altitude
263.148 km
Semi-major axis
6,645.086 km
Eccentricity
0.00057
Inclination
97.3012°
RAAN
343.7107°
Arg. of periapsis
167.5015°
True anomaly
192.62637°
Mean anomaly
192.6407°
Eccentric anomaly
192.63353°
Mean motion
4.00675 °/min
Orbital period
89.85 mins
BSTAR
0.00083577
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Computing Atmospheric mass density...

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