DECAYED

STARLINK-1399, 45683 (Decayed)

Orbit data source: Space-Track

STARLINK-1399, 45683 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.

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<iframe src="https://www.satcat.com/sats-embedded/45683?time=2025-03-26&theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

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Identifier	45683, 2020-035AC
Orbit	Decayed
Last TLE update	3 days 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, 10.11 m
Radar Cross Section	13.562 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 3 days ago

0 STARLINK-1399
1 45683U 20035AC  25082.21155325  .15653741  12538-4  39256-3 0  9990
2 45683  53.0271 153.5800 0003192 280.9960 130.4255 16.45951773266054

Epoch: 2025-03-23T05:04Z

Definitive object data (Epoch: 2025-03-23T05:04:38.2Z)

Latitude	38.7993°
Longitude	-66.52778°
Altitude	154.674 km
Speed	7.818 km/s
True Right ascension	12h 42m 18s
True Declination	38° 36' 57"
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	152.393 km
Perigee altitude	148.225 km
Semi-major axis	6,528.446 km
Eccentricity	0.0003192
Inclination	53.0271°
RAAN	153.58°
Arg. of periapsis	280.996°
True anomaly	130.45334°
Mean anomaly	130.4255°
Eccentric anomaly	130.43942°
Mean motion	4.11461 °/min
BSTAR	0.00039256
Orbital period	87.49 mins