DECAYED

STARLINK-1027, 44732 (Decayed)

Orbit data source: Space-Track

STARLINK-1027, 44732 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 11 Nov 2019 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
44732, 2019-074V
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)
2019-11-11 (6 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: 5 months ago

TLE from 5 months ago
0 STARLINK-1027
1 44732U 19074V   25117.19163693  .19662302  12507-4  39358-3 0  9994
2 44732  53.0192 130.6034 0003787 219.2663 190.0710 16.46982601301727
Epoch: 2025-04-27T04:35Z
TLE epoch observation values (Epoch: 2025-04-27T04:35:57.43Z)
Latitude
37.42057°
Longitude
-118.86097°
Altitude
152.751 km
Speed
7.818 km/s
True Right ascension
11h 02m 12s
True Declination
37° 14' 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
00:26:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
150.058 km
Perigee altitude
145.115 km
Semi-major axis
6,525.723 km
Eccentricity
0.00038
Inclination
53.0192°
RAAN
130.6034°
Arg. of periapsis
219.2663°
True anomaly
190.06341°
Mean anomaly
190.071°
Eccentric anomaly
190.06721°
Mean motion
4.11718 °/min
Orbital period
87.44 mins
BSTAR
0.00039358
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Computing Atmospheric mass density...

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