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 (2 years 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: 3 days ago

TLE from 3 days ago
0 FALCON HEAVY R/B
1 60134U 24119B   26154.92747261 -.00000088  00000-0  00000-0 0  9994
2 60134   5.8717  67.3874 2954880 238.5917  88.9668  1.51715377 10755
Epoch: 2026-06-03T22:15Z
TLE epoch observation values (Epoch: 2026-06-03T22:15:33.633Z)
Latitude
0.00001°
Longitude
-159.06081°
Altitude
28,135.58 km
Speed
3.262 km/s
True Right ascension
04h 28m 50s
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
03:29:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,069.858 km
Perigee altitude
16,162.103 km
Semi-major axis
31,994.118 km
Eccentricity
0.29549
Inclination
5.8717°
RAAN
67.3874°
Arg. of periapsis
238.5917°
True anomaly
121.25611°
Mean anomaly
88.9668°
Eccentric anomaly
105.29718°
Mean motion
0.37926 °/min
Orbital period
949.21 mins
BSTAR
0
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Other satellites on launch #119 in the year 2024 (2024-06-25 UTC)

Documentation

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