DECAYED

STARLINK-1233, 45214 (Decayed)

Orbit data source: Space-Track

STARLINK-1233, 45214 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-1233 details

Identifier	45214, 2020-012AN
Orbit	Decayed
Last TLE update	4 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 4 months ago

0 STARLINK-1233
1 45214U 20012AN  24251.52473556  .12068549  11960-4  40922-2 0  9997
2 45214  53.0419 250.7743 0000964  42.3125  47.8914 16.24868836252626

Epoch: 2024-09-07T12:35Z

Definitive object data (Epoch: 2024-09-07T12:35:37.152Z)

Latitude	53.19921°
Longitude	165.14096°
Altitude	212.428 km
Speed	7.786 km/s
True Right ascension	22h 44m 30s
True Declination	53° 01' 13"
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	207.287 km
Perigee altitude	206.017 km
Semi-major axis	6,584.789 km
Eccentricity	0.0000964
Inclination	53.0419°
RAAN	250.7743°
Arg. of periapsis	42.3125°
True anomaly	47.8996°
Mean anomaly	47.8914°
Eccentric anomaly	47.8955°
Mean motion	4.06191 °/min
BSTAR	0.0040922
Orbital period	88.63 mins