FALCON 9 R/B, 44480

Orbit data source: Space-Track

FALCON 9 R/B, 44480 is space debris in HEO originally from a launch on Tue, 06 Aug 2019 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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FALCON 9 R/B details

Identifier	44480, 2019-050B
Orbit	HEO
Last TLE update	5 hours ago
Origin	SpaceX (US)
Manufacturer	SpaceX
Mission	Spacecraft
Bus & Motor	F9ST2, Unknown motor
Mass	~4,000 kg wet, ~4,000 kg dry
Launch date (UTC)	2019-08-06 (5 years ago)
Launch vehicle	Unknown
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl, 15.53 m
Radar Cross Section	39.980 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 5 hours ago

0 FALCON 9 R/B
1 44480U 19050B   24337.10601563  .00115495  15352-6  20794-2 0  9997
2 44480  26.0737 219.3095 6167595  59.7845 347.0855  3.87972913 56511

Epoch: 2024-12-02T02:32Z

Definitive object data (Epoch: 2024-12-02T02:32:39.75Z)

Latitude	-0.00001°
Longitude	109.76415°
Altitude	1,697.48 km
Speed	8.684 km/s
True Right ascension	14h 37m 27s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-25.39154°
Longitude	34.20993°
Altitude	12,878.979 km
Speed	4.255 km/s
Apparent Right ascension	10h 38m 41s
Apparent Declination	-38° 20' 25"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	05:34:00
Azimuth	128.049° SE
Elevation	-14.73°
Doppler factor	1

Orbital elements

Apogee altitude	21,287.569 km
Perigee altitude	179.807 km
Semi-major axis	17,111.825 km
Eccentricity	0.6167595
Inclination	26.0737°
RAAN	219.3095°
Arg. of periapsis	59.7845°
True anomaly	300.26222°
Mean anomaly	347.0855°
Eccentric anomaly	328.75685°
Mean motion	0.96961 °/min
BSTAR	0.0020794
Orbital period	371.28 mins