DECAYED

STARLINK-1690, 46358 (Decayed)

Orbit data source: Space-Track

STARLINK-1690, 46358 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 03 Sep 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-1690 details

Identifier	46358, 2020-062AK
Orbit	Decayed
Last TLE update	2 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)	2020-09-03 (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 2 months ago

0 STARLINK-1690
1 46358U 20062AK  24303.40461185  .14712205  12356-4  16703-2 0  9999
2 46358  53.0229  57.5888 0008607 314.8805 156.7359 16.36058045230065

Epoch: 2024-10-29T09:42Z

Definitive object data (Epoch: 2024-10-29T09:42:38.463Z)

Latitude	48.09683°
Longitude	-2.82536°
Altitude	186.823 km
Speed	7.797 km/s
True Right ascension	12h 04m 12s
True Declination	47° 54' 39"
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	182.242 km
Perigee altitude	170.959 km
Semi-major axis	6,554.738 km
Eccentricity	0.0008607
Inclination	53.0229°
RAAN	57.5888°
Arg. of periapsis	314.8805°
True anomaly	156.77482°
Mean anomaly	156.7359°
Eccentric anomaly	156.75536°
Mean motion	4.08988 °/min
BSTAR	0.0016703
Orbital period	88.02 mins