FALCON 9 R/B, 58996

Orbit data source: Space-Track

FALCON 9 R/B, 58996 is space debris in HEO originally from a launch on Tue, 20 Feb 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	58996, 2024-035B
Orbit	HEO
Last TLE update	2 days 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)	2024-02-20 (10 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 2 days ago

0 FALCON 9 R/B
1 58996U 24035B   24355.42459040 -.00000017  00000-0  14698-3 0  9998
2 58996  19.1529 218.3048 7967733 303.4027   4.5034  1.39499415  4211

Epoch: 2024-12-20T10:11Z

Definitive object data (Epoch: 2024-12-20T10:11:24.61Z)

Latitude	0.00228°
Longitude	-23.69369°
Altitude	2,284.332 km
Speed	8.958 km/s
True Right ascension	14h 34m 35s
True Declination	0° 00' 08"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	14.65399°
Longitude	106.81747°
Altitude	53,280.816 km
Speed	1.258 km/s
Apparent Right ascension	22h 57m 20s
Apparent Declination	10° 43' 18"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	05:27:21
Azimuth	283.009° WNW
Elevation	1.199°
Doppler factor	1

Orbital elements

Apogee altitude	54,422.851 km
Perigee altitude	498.849 km
Semi-major axis	33,838.987 km
Eccentricity	0.7967733
Inclination	19.1529°
RAAN	218.3048°
Arg. of periapsis	303.4027°
True anomaly	56.44747°
Mean anomaly	4.5034°
Eccentric anomaly	20.46443°
Mean motion	0.34867 °/min
BSTAR	0.00014698
Orbital period	1032.49 mins