DECAYED

STARLINK-1401, 45684 (Decayed)

Orbit data source: Space-Track

STARLINK-1401, 45684 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

Identifier	45684, 2020-035AD
Orbit	Decayed
Last TLE update	1 month 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 1 month ago

0 STARLINK-1401
1 45684U 20035AD  25038.07151361  .14445581  12558-4  31795-3 0  9994
2 45684  53.0249 267.5928 0007512 281.4100 233.6070 16.46124799260594

Epoch: 2025-02-07T01:42Z

Definitive object data (Epoch: 2025-02-07T01:42:58.775Z)

Latitude	19.81617°
Longitude	-91.23908°
Altitude	152.938 km
Speed	7.816 km/s
True Right ascension	04h 47m 46s
True Declination	19° 41' 48"
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	154.756 km
Perigee altitude	144.948 km
Semi-major axis	6,527.989 km
Eccentricity	0.0007512
Inclination	53.0249°
RAAN	267.5928°
Arg. of periapsis	281.41°
True anomaly	233.53775°
Mean anomaly	233.607°
Eccentric anomaly	233.57237°
Mean motion	4.11504 °/min
BSTAR	0.00031795
Orbital period	87.48 mins