FALCON HEAVY R/B, 60134

Orbit data source: Space-Track

FALCON HEAVY R/B, 60134 is space debris in HEO originally from a launch on Tue, 25 Jun 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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Identifier
60134, 2024-119B
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)
2024-06-25 (1 year ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, Unknown HBR
Radar Cross Section
49.816 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 FALCON HEAVY R/B
1 60134U 24119B   25341.33512653 -.00000102  00000-0  00000-0 0  9998
2 60134   5.5290  73.8987 2975039 224.0708 107.7401  1.51715036  8048
Epoch: 2025-12-07T08:02Z
TLE epoch observation values (Epoch: 2025-12-07T08:02:34.932Z)
Latitude
0.00001°
Longitude
-123.28807°
Altitude
30,709.978 km
Speed
3.006 km/s
True Right ascension
04h 54m 49s
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
02:41:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,134.425 km
Perigee altitude
16,097.644 km
Semi-major axis
31,994.171 km
Eccentricity
0.2975
Inclination
5.529°
RAAN
73.8987°
Arg. of periapsis
224.0708°
True anomaly
135.76137°
Mean anomaly
107.7401°
Eccentric anomaly
122.16898°
Mean motion
0.37926 °/min
Orbital period
949.22 mins
BSTAR
0
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Other satellites on launch #119 in the year 2024 (2024-06-25 UTC)

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