FALCON 9 R/B, 59347

Orbit data source: Space-Track

FALCON 9 R/B, 59347 is space debris in HEO originally from a launch on Sat, 30 Mar 2024 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	59347, 2024-059B
Orbit	HEO
Last TLE update	1 day 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)	2024-03-30 (9 months 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 1 day ago

0 FALCON 9 R/B
1 59347U 24059B   24355.22502450  .00000110  00000-0  10195-2 0  9997
2 59347  25.5809 301.0837 8163196 259.5961  10.9742  1.24120774  3253

Epoch: 2024-12-20T05:24Z

Definitive object data (Epoch: 2024-12-20T05:24:02.116Z)

Latitude	0°
Longitude	130.76477°
Altitude	7,999.523 km
Speed	6.674 km/s
True Right ascension	20h 04m 16s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	24.2815°
Longitude	-119.83419°
Altitude	37,706.319 km
Speed	2.681 km/s
Apparent Right ascension	03h 21m 45s
Apparent Declination	17° 17' 54"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	15:20:52
Azimuth	359.746° N
Elevation	-32.785°
Doppler factor	1

Orbital elements

Apogee altitude	60,060.112 km
Perigee altitude	340.617 km
Semi-major axis	36,578.502 km
Eccentricity	0.8163196
Inclination	25.5809°
RAAN	301.0837°
Arg. of periapsis	259.5961°
True anomaly	101.71443°
Mean anomaly	10.9742°
Eccentric anomaly	42.68215°
Mean motion	0.31024 °/min
BSTAR	0.0010195
Orbital period	1160.37 mins