FALCON 9 R/B, 62029 (Decayed)
Orbit data source: Space-Track
FALCON 9 R/B, 62029 was space debris in LEO originally from a launch on Mon, 18 Nov 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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62029 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX
Mission
Decayed 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, 7.8 m
Radar Cross Section
39.980 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 FALCON 9 R/B
1 62029U 24214B 25103.96199847 .00002311 -72994-5 00000+0 0 9999
2 62029 27.6609 124.9151 0788001 251.9017 176.7563 14.75115204 2268Epoch: 2025-04-13T23:05Z
TLE epoch observation values (Epoch: 2025-04-13T23:05:16.667Z)
Latitude
25.81503°
Longitude
2.89672°
Altitude
1,195.646 km
Speed
6.97 km/s
True Right ascension
12h 46m 23s
True Declination
25° 41' 18"
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
08:33:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,202.821 km
Perigee altitude
95.33 km
Semi-major axis
7,027.213 km
Eccentricity
0.0788
Inclination
27.6609°
RAAN
124.9151°
Arg. of periapsis
251.9017°
True anomaly
177.22134°
Mean anomaly
176.7563°
Eccentric anomaly
176.99313°
Mean motion
3.68441 °/min
Orbital period
97.71 mins
BSTAR
0
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Other satellites on launch #214 in the year 2024 (2024-11-18 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.FALCON 9 R/B Visibility
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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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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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