DECAYED

STARLINK-1617, 46350 (Decayed)

Orbit data source: Space-Track

STARLINK-1617, 46350 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 03 Sep 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-1617 details

Identifier	46350, 2020-062AB
Orbit	Decayed
Last TLE update	7 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)	2020-09-03 (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 7 months ago

0 STARLINK-1617
1 46350U 20062AB  24159.67309141  .27472704  12265-4  39212-2 0  9992
2 46350  53.0306 321.1677 0014437 288.1110 177.6355 16.33671739208701

Epoch: 2024-06-07T16:09Z

Definitive object data (Epoch: 2024-06-07T16:09:15.097Z)

Latitude	50.415°
Longitude	-62.53659°
Altitude	198.01 km
Speed	7.788 km/s
True Right ascension	05h 05m 17s
True Declination	50° 13' 54"
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	192.452 km
Perigee altitude	173.508 km
Semi-major axis	6,561.117 km
Eccentricity	0.0014437
Inclination	53.0306°
RAAN	321.1677°
Arg. of periapsis	288.111°
True anomaly	177.64231°
Mean anomaly	177.6355°
Eccentric anomaly	177.63891°
Mean motion	4.08391 °/min
BSTAR	0.0039212
Orbital period	88.15 mins