DECAYED

STARLINK-1421, 45709 (Decayed)

Orbit data source: Space-Track

STARLINK-1421, 45709 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

STARLINK-1421 details

Identifier	45709, 2020-035BE
Orbit	Decayed
Last TLE update	3 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)	2020-06-04 (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, 8.86 m
Radar Cross Section	13.562 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 3 months ago

0 STARLINK-1421
1 45709U 20035BE  24241.78069622  .14500711  12048-4  55493-2 0  9994
2 45709  53.0312 308.5036 0008968 341.5215 122.8771 16.23304678235668

Epoch: 2024-08-28T18:44Z

Definitive object data (Epoch: 2024-08-28T18:44:12.153Z)

Latitude	50.83085°
Longitude	163.2479°
Altitude	219.76 km
Speed	7.779 km/s
True Right ascension	04h 07m 06s
True Declination	50° 38' 55"
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	216.792 km
Perigee altitude	204.974 km
Semi-major axis	6,589.02 km
Eccentricity	0.0008968
Inclination	53.0312°
RAAN	308.5036°
Arg. of periapsis	341.5215°
True anomaly	122.96335°
Mean anomaly	122.8771°
Eccentric anomaly	122.92023°
Mean motion	4.058 °/min
BSTAR	0.0055493
Orbital period	88.71 mins