DECAYED

STARLINK-1729, 46583 (Decayed)

Orbit data source: Space-Track

STARLINK-1729, 46583 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 06 Oct 2020 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft 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
Identifier
46583, 2020-070BD
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Decayed Commercial Communications
Bus & Motor
STARLINK, Unknown motor
Mass
260 kg wet, ~248 kg dry
Launch date (UTC)
2020-10-06 (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, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 months ago

TLE from 9 months ago
0 STARLINK-1729
1 46583U 20070BD  25031.31128911  .28859392  12867-4  25766-3 0  9995
2 46583  53.0335 147.5218 0014459 328.5633 115.6036 16.50583367239367
Epoch: 2025-01-31T07:28Z
TLE epoch observation values (Epoch: 2025-01-31T07:28:15.379Z)
Latitude
52.81972°
Longitude
-14.72667°
Altitude
148.272 km
Speed
7.821 km/s
True Right ascension
15h 12m 27s
True Declination
52° 38' 19"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
03:20:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
147.512 km
Perigee altitude
128.669 km
Semi-major axis
6,516.228 km
Eccentricity
0.00145
Inclination
53.0335°
RAAN
147.5218°
Arg. of periapsis
328.5633°
True anomaly
115.7529°
Mean anomaly
115.6036°
Eccentric anomaly
115.67826°
Mean motion
4.12619 °/min
Orbital period
87.25 mins
BSTAR
0.00025766
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|