Showing default

CENTAURI-1, 43809

Orbit data source: Space-Track

CENTAURI-1, 43809 is a payload satellite owned by Fleet Space (AU) in SSO that was launched on Mon, 03 Dec 2018 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
43809, 2018-099BD
Orbit
SSO
Country
Flag of AUAU / AUS
Related business
Manufacturer
Fleet Space
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
2018-12-03 (8 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 CENTAURI-1
1 43809U 18099BD  26170.71362783  .00003930  00000-0  20546-3 0  9999
2 43809  97.4214 222.3792 0012831 324.2306  35.8066 15.16385455412889
Epoch: 2026-06-19T17:07Z
TLE epoch observation values (Epoch: 2026-06-19T17:07:37.444Z)
Latitude
-0.00008°
Longitude
57.53454°
Altitude
512.688 km
Speed
7.611 km/s
True Right ascension
14h 49m 31s
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
21:35:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
522.59 km
Perigee altitude
504.904 km
Semi-major axis
6,891.884 km
Eccentricity
0.00128
Inclination
97.4214°
RAAN
222.3792°
Arg. of periapsis
324.2306°
True anomaly
35.89273°
Mean anomaly
35.8066°
Eccentric anomaly
35.84966°
Mean motion
3.79347 °/min
Orbital period
94.9 mins
BSTAR
0.00020546
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
|