FALCON 9 R/B, 43612

Orbit data source: Space-Track

FALCON 9 R/B, 43612 is space debris in HEO originally from a launch on Mon, 10 Sep 2018 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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Identifier
43612, 2018-069B
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
SpaceX
Mission
Spacecraft
Bus & Motor
F9ST2, Unknown motor
Mass
~4,000 kg wet, ~4,000 kg dry
Launch date (UTC)
2018-09-10 (7 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 7.8 m
Radar Cross Section
39.980 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 FALCON 9 R/B
1 43612U 18069B   25260.51711392  .00028607  00000-0  21105-2 0  9998
2 43612  27.0963  45.6551 5398265 153.3153 249.6337  5.02489228119780
Epoch: 2025-09-17T12:24Z
TLE epoch observation values (Epoch: 2025-09-17T12:24:38.642Z)
Latitude
-0.00003°
Longitude
-137.19487°
Altitude
13,318.751 km
Speed
3.577 km/s
True Right ascension
03h 02m 37s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
11:05:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
15,798.513 km
Perigee altitude
249.302 km
Semi-major axis
14,402.045 km
Eccentricity
0.53983
Inclination
27.0963°
RAAN
45.6551°
Arg. of periapsis
153.3153°
True anomaly
206.74788°
Mean anomaly
249.6337°
Eccentric anomaly
227.00957°
Mean motion
1.25576 °/min
Orbital period
286.68 mins
BSTAR
0.0021105
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Other satellites on launch #69 in the year 2018 (2018-09-10 UTC)

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