Showing default

FALCONSAT-6, 43815

Orbit data source: Space-Track

FALCONSAT-6, 43815 is a payload satellite owned by USAF SMC (US) 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
43815, 2018-099BK
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
USAF Academy
Mission
Operational Defense Technology
Bus & Motor
FALCONSAT, Unknown motor
Mass
181 kg wet, 181 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 + 1 Ant, 2.0 m
Radar Cross Section
0.551 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 FALCONSAT-6
1 43815U 18099BK  26244.78180632  .00002326  00000-0  88265-4 0  9997
2 43815  97.3746 319.9742 0016090  36.5596  80.1423 15.27751358425423
Epoch: 2026-09-01T18:45Z
TLE epoch observation values (Epoch: 2026-09-01T18:45:48.066Z)
Latitude
62.29334°
Longitude
-108.23259°
Altitude
491.378 km
Speed
7.626 km/s
True Right ascension
10h 16m 38s
True Declination
62° 08' 46"
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
23:38:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.524 km
Perigee altitude
468.456 km
Semi-major axis
6,857.627 km
Eccentricity
0.00161
Inclination
97.3746°
RAAN
319.9742°
Arg. of periapsis
36.5596°
True anomaly
80.32402°
Mean anomaly
80.1423°
Eccentric anomaly
80.23315°
Mean motion
3.82193 °/min
Orbital period
94.19 mins
BSTAR
0.000088265
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|