DECAYED

STARLINK-1415, 45691 (Decayed)

Orbit data source: Space-Track

STARLINK-1415, 45691 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-1415 details

Identifier	45691, 2020-035AL
Orbit	Decayed
Last TLE update	5 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 5 months ago

0 STARLINK-1415
1 45691U 20035AL  24223.06158267  .28350328  12304-4  32730-2 0  9995
2 45691  53.0476  65.5010 0005795 303.4245 189.2394 16.35988559232761

Epoch: 2024-08-10T01:28Z

Definitive object data (Epoch: 2024-08-10T01:28:40.742Z)

Latitude	36.11881°
Longitude	-128.77359°
Altitude	183.018 km
Speed	7.799 km/s
True Right ascension	14h 09m 41s
True Declination	35° 56' 27"
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	180.581 km
Perigee altitude	172.983 km
Semi-major axis	6,554.919 km
Eccentricity	0.0005795
Inclination	53.0476°
RAAN	65.501°
Arg. of periapsis	303.4245°
True anomaly	189.22875°
Mean anomaly	189.2394°
Eccentric anomaly	189.23407°
Mean motion	4.08971 °/min
BSTAR	0.003273
Orbital period	88.03 mins