DECAYED

STARLINK-1416, 45692 (Decayed)

Orbit data source: Space-Track

STARLINK-1416, 45692 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 04 Jun 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-1416 details

Identifier	45692, 2020-035AM
Orbit	Decayed
Last TLE update	3 months 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)	2020-06-04 (5 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 3 months ago

0 STARLINK-1416
1 45692U 20035AM  24266.97909852  .49721084  12363-4  32775-2 0  9995
2 45692  53.0277 256.5784 0002116 219.3664 244.6748 16.40832200238611

Epoch: 2024-09-22T23:29Z

Definitive object data (Epoch: 2024-09-22T23:29:54.112Z)

Latitude	50.97356°
Longitude	14.35955°
Altitude	170.16 km
Speed	7.81 km/s
True Right ascension	00h 36m 35s
True Declination	50° 47' 24"
Sunlit	Object was in full shadow 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	165.265 km
Perigee altitude	162.496 km
Semi-major axis	6,542.017 km
Eccentricity	0.0002116
Inclination	53.0277°
RAAN	256.5784°
Arg. of periapsis	219.3664°
True anomaly	244.65289°
Mean anomaly	244.6748°
Eccentric anomaly	244.66384°
Mean motion	4.10181 °/min
BSTAR	0.0032775
Orbital period	87.77 mins