DECAYED

STARLINK-1826, 46723 (Decayed)

Orbit data source: Space-Track

STARLINK-1826, 46723 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 18 Oct 2020 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
46723, 2020-073BF
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Decayed Commercial Communications
Bus & Motor
STARLINK, Unknown motor
Mass
260 kg wet, ~248 kg dry
Launch date (UTC)
2020-10-18 (6 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 month ago

TLE from 1 month ago
0 STARLINK-1826
1 46723U 20073BF  26217.20537272  .04733989  12147-4  75286-3 0  9993
2 46723  53.0218 156.3619 0005766 245.3369 114.7074 16.32965134321459
Epoch: 2026-08-05T04:55Z
TLE epoch observation values (Epoch: 2026-08-05T04:55:44.203Z)
Latitude
Longitude
128.66461°
Altitude
187.091 km
Speed
7.794 km/s
True Right ascension
10h 25m 26s
True Declination
0° 00' 00"
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
12:04:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
188.658 km
Perigee altitude
181.09 km
Semi-major axis
6,563.011 km
Eccentricity
0.00058
Inclination
53.0218°
RAAN
156.3619°
Arg. of periapsis
245.3369°
True anomaly
114.76741°
Mean anomaly
114.7074°
Eccentric anomaly
114.73741°
Mean motion
4.08215 °/min
Orbital period
88.19 mins
BSTAR
0.00075286
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|