FALCON 9 R/B, 62007

Orbit data source: Space-Track

FALCON 9 R/B, 62007 is space debris in HEO originally from a launch on Sun, 17 Nov 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.

Loading next visibility...

FALCON 9 R/B details

Identifier	62007, 2024-212B
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)	2024-11-17 (4 days 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 2 days ago

0 FALCON 9 R/B
1 62007U 24212B   24324.55564779  .00002249  00000-0  15981-1 0  9991
2 62007  17.7833 221.1756 7828684 179.6885 181.6859  1.56377628    33

Epoch: 2024-11-19T13:20Z

Definitive object data (Epoch: 2024-11-19T13:20:07.969Z)

Latitude	0.0002°
Longitude	-37.89133°
Altitude	49,547.311 km
Speed	1.242 km/s
True Right ascension	14h 44m 49s
True Declination	0° 00' 01"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-8.31409°
Longitude	-65.32336°
Altitude	32,350.73 km
Speed	2.805 km/s
Apparent Right ascension	13h 11m 22s
Apparent Declination	-12° 52' 13"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	03:26:14
Azimuth	57.145° ENE
Elevation	-49.895°
Doppler factor	1

Orbital elements

Apogee altitude	49,529.928 km
Perigee altitude	430.783 km
Semi-major axis	31,358.492 km
Eccentricity	0.7828684
Inclination	17.7833°
RAAN	221.1756°
Arg. of periapsis	179.6885°
True anomaly	180.33001°
Mean anomaly	181.6859°
Eccentric anomaly	180.94563°
Mean motion	0.39085 °/min
BSTAR	0.015981
Orbital period	921.07 mins