FALCON HEAVY R/B, 61508
Orbit data source: Space-Track
FALCON HEAVY R/B, 61508 is space debris in LEO originally from a launch on Mon, 14 Oct 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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61508 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
10 months ago
Origin
Manufacturer
SpaceX
Mission
Spacecraft
Bus & Motor
F9ST2, Unknown motor
Mass
~4,000 kg wet, ~4,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, Unknown HBR
Radar Cross Section
49.816 m²
Expand to show TLE details & history
TLE from 10 months ago
0 FALCON HEAVY R/B
1 61508U 24182B 24288.67632810 .00000840 -26562-5 00000-0 0 9993
2 61508 31.9400 67.0176 0018900 60.7600 70.5300 16.38814738 07Epoch: 2024-10-14T16:13Z
TLE epoch observation values (Epoch: 2024-10-14T16:13:54.747Z)
Latitude
23.45054°
Longitude
-63.93444°
Altitude
163.258 km
Speed
7.816 km/s
True Right ascension
13h 32m 58s
True Declination
23° 18' 50"
Sunlit
Visualization orbit readout
Latitude
31.62674°
Longitude
50.01569°
Altitude
157.007 km
Speed
7.825 km/s
Apparent Right ascension
17h 24m 44s
Apparent Declination
-7° 57' 02"
Sunlit
Visualization observer readout
Local Sidereal Time
00:42:44
Azimuth
276.479° WNW
Elevation
-20.017°
Doppler factor
1
Orbital elements
Apogee altitude
185.247 km
Perigee altitude
160.485 km
Semi-major axis
6,551.003 km
Eccentricity
0.00189
Inclination
31.94°
RAAN
67.0176°
Arg. of periapsis
60.76°
True anomaly
70.73435°
Mean anomaly
70.53°
Eccentric anomaly
70.63216°
Mean motion
4.09337 °/min
Orbital period
87.95 mins
BSTAR
0
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Other satellites on launch #182 in the year 2024 (2024-10-14 UTC)
FALCON HEAVY R/B Visibility
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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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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Authenticating...
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