DECAYED

STARLINK-1032, 44737 (Decayed)

Orbit data source: Space-Track

STARLINK-1032, 44737 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

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<iframe src="https://www.satcat.com/sats-embedded/44737?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

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https://www.satcat.com/sats-embedded/44737?theme=dark&initialShowStats=false

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Identifier	44737, 2019-074AA
Orbit	Decayed
Last TLE update	1 week ago
Origin	SPX (US)
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 (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, 8.86 m
Radar Cross Section	13.562 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 week ago

0 STARLINK-1032
1 44737U 19074AA  25084.71487008  .09721750  12342-4  88542-3 0  9997
2 44737  53.0302 272.0337 0004997 292.5814 165.3940 16.38108285296898

Epoch: 2025-03-25T17:09Z

Definitive object data (Epoch: 2025-03-25T17:09:24.774Z)

Latitude	52.45545°
Longitude	-65.58032°
Altitude	180.32 km
Speed	7.803 km/s
True Right ascension	01h 00m 44s
True Declination	52° 16' 28"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	174.402 km
Perigee altitude	167.857 km
Semi-major axis	6,549.266 km
Eccentricity	0.0004997
Inclination	53.0302°
RAAN	272.0337°
Arg. of periapsis	292.5814°
True anomaly	165.40843°
Mean anomaly	165.394°
Eccentric anomaly	165.40122°
Mean motion	4.095 °/min
BSTAR	0.00088542
Orbital period	87.91 mins