DECAYED

STARLINK-1529, 46067 (Decayed)

Orbit data source: Space-Track

STARLINK-1529, 46067 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 07 Aug 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-1529 details

Identifier	46067, 2020-055AS
Orbit	Decayed
Last TLE update	7 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)	2020-08-07 (4 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 7 months ago

0 STARLINK-1529
1 46067U 20055AS  24113.16570227  .10537836  12480-4  87169-3 0  9992
2 46067  53.0263 213.4733 0009270 346.7704  14.4422 16.38792081206488

Epoch: 2024-04-22T03:58Z

Definitive object data (Epoch: 2024-04-22T03:58:36.676Z)

Latitude	0.91222°
Longitude	-56.2051°
Altitude	163.954 km
Speed	7.813 km/s
True Right ascension	14h 16m 37s
True Declination	0° 54' 23"
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	175.378 km
Perigee altitude	163.239 km
Semi-major axis	6,547.445 km
Eccentricity	0.000927
Inclination	53.0263°
RAAN	213.4733°
Arg. of periapsis	346.7704°
True anomaly	14.46872°
Mean anomaly	14.4422°
Eccentric anomaly	14.45546°
Mean motion	4.09671 °/min
BSTAR	0.00087169
Orbital period	87.88 mins