DECAYED

STARLINK-1007, 44713 (Decayed)

Orbit data source: Space-Track

STARLINK-1007, 44713 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). Payloads include a variety of satellites, spacecraft, and rockets 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

STARLINK-1007 details

Identifier	44713, 2019-074A
Orbit	Decayed
Last TLE update	2 months ago
Origin	SpaceX/Seattle (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 2 months ago

0 STARLINK-1007
1 44713U 19074A   24276.62104521  .27315559  12225-4  58439-2 0  9996
2 44713  53.0382 329.7306 0008324   5.1336 119.9714 16.29877576270703

Epoch: 2024-10-02T14:54Z

Definitive object data (Epoch: 2024-10-02T14:54:18.306Z)

Latitude	40.90739°
Longitude	-126.07527°
Altitude	199.353 km
Speed	7.791 km/s
True Right ascension	07h 17m 16s
True Declination	40° 43' 22"
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	198.626 km
Perigee altitude	187.686 km
Semi-major axis	6,571.293 km
Eccentricity	0.0008324
Inclination	53.0382°
RAAN	329.7306°
Arg. of periapsis	5.1336°
True anomaly	120.05399°
Mean anomaly	119.9714°
Eccentric anomaly	120.0127°
Mean motion	4.07443 °/min
BSTAR	0.0058439
Orbital period	88.36 mins