DECAYED

STARLINK-1916, 46766 (Decayed)

Orbit data source: Space-Track

STARLINK-1916, 46766 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 24 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
46766, 2020-074AD
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)
2020-10-24 (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, 4.4 m
Radar Cross Section
13.562 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 4 months ago

TLE from 4 months ago
0 STARLINK-1916
1 46766U 20074AD  25108.03380811  .18205412  12574-4  49910-3 0  9994
2 46766  53.0333 319.1419 0009108 299.7938 193.1024 16.44866309247663
Epoch: 2025-04-18T00:48Z
TLE epoch observation values (Epoch: 2025-04-18T00:48:41.02Z)
Latitude
35.96392°
Longitude
-112.3114°
Altitude
161.424 km
Speed
7.811 km/s
True Right ascension
07h 05m 01s
True Declination
35° 47' 08"
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
23:57:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
159.128 km
Perigee altitude
147.231 km
Semi-major axis
6,531.317 km
Eccentricity
0.00091
Inclination
53.0333°
RAAN
319.1419°
Arg. of periapsis
299.7938°
True anomaly
193.07877°
Mean anomaly
193.1024°
Eccentric anomaly
193.09058°
Mean motion
4.1119 °/min
Orbital period
87.55 mins
BSTAR
0.0004991
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|