FALCON 9 R/B, 61732

Orbit data source: Space-Track

FALCON 9 R/B, 61732 is space debris in LEO originally from a launch on Mon, 07 Oct 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.

Not visible in the next 10 days

FALCON 9 R/B details

Identifier	61732, 2024-180B
Orbit	LEO
Last TLE update	3 months 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)	2024-10-07 (3 months ago)
Launch vehicle	Unknown
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	RCS unknown

Expand to show TLE details & history

TLE from 3 months ago

0 FALCON 9 R/B
1 61732U 24180B   24281.62491802 -.00000101  32184-6  00000-0 0  9990
2 61732  34.1400  34.7539 0027900 134.8400 359.2800 16.36805402    04

Epoch: 2024-10-07T14:59Z

Definitive object data (Epoch: 2024-10-07T14:59:52.916Z)

Latitude	23.8652°
Longitude	-67.40956°
Altitude	154.724 km
Speed	7.829 km/s
True Right ascension	11h 37m 14s
True Declination	23° 43' 35"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-27.98366°
Longitude	-170.69542°
Altitude	165.987 km
Speed	7.816 km/s
Apparent Right ascension	05h 06m 15s
Apparent Declination	-33° 50' 44"
Sunlit	Object is in full shadow

Visualization observer readout

Local Sidereal Time	17:32:26
Azimuth	42.787° NE
Elevation	-81.989°
Doppler factor	1

Orbital elements

Apogee altitude	196.157 km
Perigee altitude	159.575 km
Semi-major axis	6,556.003 km
Eccentricity	0.00279
Inclination	34.14°
RAAN	34.7539°
Arg. of periapsis	134.84°
True anomaly	359.27597°
Mean anomaly	359.28°
Eccentric anomaly	359.27799°
Mean motion	4.08869 °/min
BSTAR	Unknown
Orbital period	88.05 mins