FALCON 9 R/B, 61911

Orbit data source: Space-Track

FALCON 9 R/B, 61911 is space debris originally from a launch on Mon, 11 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.

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FALCON 9 R/B details

Identifier	61911, 2024-206B
Orbit	Molniya
Last TLE update	10 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)	2024-11-11 (1 month ago)
Launch vehicle	Unknown
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 10 hours ago

0 FALCON 9 R/B
1 61911U 24206B   24348.53811750  .00003813  00000-0  20045-2 0  9991
2 61911  27.0397 136.5592 7246082 198.6015 106.3345  2.30658489   735

Epoch: 2024-12-13T12:54Z

Definitive object data (Epoch: 2024-12-13T12:54:53.352Z)

Latitude	-0.00002°
Longitude	-139.93538°
Altitude	30,309.196 km
Speed	2.293 km/s
True Right ascension	09h 05m 57s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-1.08851°
Longitude	-142.23176°
Altitude	29,018.697 km
Speed	2.459 km/s
Apparent Right ascension	09h 01m 34s
Apparent Declination	-6° 43' 27"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	21:36:20
Azimuth	15.533° NNE
Elevation	-55.903°
Doppler factor	1

Orbital elements

Apogee altitude	35,358.277 km
Perigee altitude	286.488 km
Semi-major axis	24,200.519 km
Eccentricity	0.7246082
Inclination	27.0397°
RAAN	136.5592°
Arg. of periapsis	198.6015°
True anomaly	161.41083°
Mean anomaly	106.3345°
Eccentric anomaly	135.45658°
Mean motion	0.57651 °/min
BSTAR	0.0020045
Orbital period	624.45 mins