DECAYED

STARLINK-1696, 46545 (Decayed)

Orbit data source: Space-Track

STARLINK-1696, 46545 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
46545, 2020-070P
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: 10 months ago

TLE from 10 months ago
0 STARLINK-1696
1 46545U 20070P   25119.02373756  .21375455  12516-4  45925-3 0  9993
2 46545  53.0179 105.6885 0005323 252.4592 221.6678 16.46478098252684
Epoch: 2025-04-29T00:34Z
TLE epoch observation values (Epoch: 2025-04-29T00:34:10.925Z)
Latitude
46.97682°
Longitude
6.56748°
Altitude
156.296 km
Speed
7.817 km/s
True Right ascension
15h 29m 22s
True Declination
46° 47' 22"
Sunlit
Object was in full shadow 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
21:53:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
152.394 km
Perigee altitude
145.445 km
Semi-major axis
6,527.056 km
Eccentricity
0.00053
Inclination
53.0179°
RAAN
105.6885°
Arg. of periapsis
252.4592°
True anomaly
221.62727°
Mean anomaly
221.6678°
Eccentric anomaly
221.64753°
Mean motion
4.11592 °/min
Orbital period
87.47 mins
BSTAR
0.00045925
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Computing Atmospheric mass density...

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