DECAYED

STARLINK-1755, 46591 (Decayed)

Orbit data source: Space-Track

STARLINK-1755, 46591 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
46591, 2020-070BM
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-1755
1 46591U 20070BM  25054.33397196  .10907526  12374-4  82297-3 0  9993
2 46591  53.0275  11.5065 0001102 356.8762  80.6842 16.39746537243286
Epoch: 2025-02-23T08:00Z
TLE epoch observation values (Epoch: 2025-02-23T08:00:55.177Z)
Latitude
51.43661°
Longitude
167.6635°
Altitude
172.443 km
Speed
7.809 km/s
True Right ascension
05h 25m 26s
True Declination
51° 15' 14"
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
04:36:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167.489 km
Perigee altitude
166.046 km
Semi-major axis
6,544.904 km
Eccentricity
0.00011
Inclination
53.0275°
RAAN
11.5065°
Arg. of periapsis
356.8762°
True anomaly
80.69666°
Mean anomaly
80.6842°
Eccentric anomaly
80.69043°
Mean motion
4.0991 °/min
Orbital period
87.82 mins
BSTAR
0.00082297
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Computing Atmospheric mass density...

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