DECAYED

STARLINK-1620, 46149 (Decayed)

Orbit data source: Space-Track

STARLINK-1620, 46149 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 18 Aug 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-1620 details

Identifier	46149, 2020-057AJ
Orbit	Decayed
Last TLE update	2 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)	2020-08-18 (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 2 months ago

0 STARLINK-1620
1 46149U 20057AJ  24310.11560671  .45994898  12375-4  33579-2 0  9992
2 46149  53.0028 301.9124 0003132  75.6773   4.4893 16.39994273233670

Epoch: 2024-11-05T02:46Z

Definitive object data (Epoch: 2024-11-05T02:46:28.419Z)

Latitude	52.05817°
Longitude	-70.61957°
Altitude	169.995 km
Speed	7.812 km/s
True Right ascension	01h 03m 19s
True Declination	51° 52' 35"
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	168.162 km
Perigee altitude	164.063 km
Semi-major axis	6,544.25 km
Eccentricity	0.0003132
Inclination	53.0028°
RAAN	301.9124°
Arg. of periapsis	75.6773°
True anomaly	4.49211°
Mean anomaly	4.4893°
Eccentric anomaly	4.49071°
Mean motion	4.09971 °/min
BSTAR	0.0033579
Orbital period	87.81 mins