DECAYED

STARLINK-1923, 46754 (Decayed)

Orbit data source: Space-Track

STARLINK-1923, 46754 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 24 Oct 2020 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets 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

STARLINK-1923 details

Identifier	46754, 2020-074R
Orbit	Decayed
Last TLE update	4 weeks ago
Origin	SpaceX/Seattle (US)
Manufacturer	SpaceX/Seattle
Mission	Decayed Commercial Communications
Bus & Motor	STARLINK, Unknown motor
Mass	260 kg wet, ~248 kg dry
Launch date (UTC)	2020-10-24 (4 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, 8.86 m
Radar Cross Section	13.562 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 4 weeks ago

0 STARLINK-1923
1 46754U 20074R   24336.92810682  .12800429  12208-4  11940-2 0  9993
2 46754  53.0296 206.0431 0007043 216.4365 245.0377 16.37847989227393

Epoch: 2024-12-01T22:16Z

Definitive object data (Epoch: 2024-12-01T22:16:28.429Z)

Latitude	51.71006°
Longitude	-90.77717°
Altitude	179.629 km
Speed	7.804 km/s
True Right ascension	20h 58m 24s
True Declination	51° 31' 40"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	176.437 km
Perigee altitude	167.21 km
Semi-major axis	6,549.96 km
Eccentricity	0.0007043
Inclination	53.0296°
RAAN	206.0431°
Arg. of periapsis	216.4365°
True anomaly	244.96456°
Mean anomaly	245.0377°
Eccentric anomaly	245.00113°
Mean motion	4.09435 °/min
BSTAR	0.001194
Orbital period	87.93 mins