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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60134 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 FALCON HEAVY R/B
1 60134U 24119B 25241.16875752 -.00000107 00000-0 00000-0 0 9995
2 60134 5.3168 77.6367 2982270 215.9352 119.9687 1.51715512 6524
Epoch: 2025-08-29T04:03Z
TLE epoch observation values (Epoch: 2025-08-29T04:03:00.649Z)
Latitude
0°
Longitude
39.42066°
Altitude
32,047.616 km
Speed
2.879 km/s
True Right ascension
05h 11m 10s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
14:27:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,157.477 km
Perigee altitude
16,074.464 km
Semi-major axis
31,994.107 km
Eccentricity
0.29823
Inclination
5.3168°
RAAN
77.6367°
Arg. of periapsis
215.9352°
True anomaly
144.19037°
Mean anomaly
119.9687°
Eccentric anomaly
132.55548°
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)
FALCON HEAVY R/B Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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923 mins | 2025-08-30 05:47:09.928Z | 244.663° WSW | 2025-08-30 16:56:09.928Z | 146.104° SSE | 34.531° | 2025-08-30 21:10:09.928Z | 111.994° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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