DECAYED

STARLINK-1574, 46062 (Decayed)

Orbit data source: Space-Track

STARLINK-1574, 46062 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 07 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.

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Identifier	46062, 2020-055AM
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)	2020-08-07 (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, 10.11 m
Radar Cross Section	13.562 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 2 months ago

0 STARLINK-1574
1 46062U 20055AM  25010.79598131  .09683813  12357-4  85402-3 0  9993
2 46062  53.0288 192.7292 0003549 310.9876 176.3379 16.38411511245056

Epoch: 2025-01-10T19:06Z

Definitive object data (Epoch: 2025-01-10T19:06:12.785Z)

Latitude	39.57568°
Longitude	-62.59496°
Altitude	175.817 km
Speed	7.805 km/s
True Right ascension	22h 18m 03s
True Declination	39° 23' 31"
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	172.646 km
Perigee altitude	167.998 km
Semi-major axis	6,548.459 km
Eccentricity	0.0003549
Inclination	53.0288°
RAAN	192.7292°
Arg. of periapsis	310.9876°
True anomaly	176.3405°
Mean anomaly	176.3379°
Eccentric anomaly	176.3392°
Mean motion	4.09576 °/min
BSTAR	0.00085402
Orbital period	87.9 mins