DECAYED

STARLINK-1245, 45215 (Decayed)

Orbit data source: Space-Track

STARLINK-1245, 45215 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 17 Feb 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-1245 details

Identifier	45215, 2020-012AP
Orbit	Decayed
Last TLE update	6 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)	2020-02-17 (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 6 months ago

0 STARLINK-1245
1 45215U 20012AP  24176.50148634  .07957224  11949-4  36648-2 0  9996
2 45215  53.0360 243.2382 0009599 338.9335 156.6525 16.21008310241050

Epoch: 2024-06-24T12:02Z

Definitive object data (Epoch: 2024-06-24T12:02:08.419Z)

Latitude	34.08292°
Longitude	-60.84925°
Altitude	225.018 km
Speed	7.773 km/s
True Right ascension	02h 11m 17s
True Declination	33° 54' 38"
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	223.433 km
Perigee altitude	210.772 km
Semi-major axis	6,595.24 km
Eccentricity	0.0009599
Inclination	53.036°
RAAN	243.2382°
Arg. of periapsis	338.9335°
True anomaly	156.69604°
Mean anomaly	156.6525°
Eccentric anomaly	156.67428°
Mean motion	4.05226 °/min
BSTAR	0.0036648
Orbital period	88.84 mins