FALCON HEAVY R/B, 100533 (Decayed)
Orbit data source: Space-Track
FALCON HEAVY R/B, 100533 was space debris in LEO originally from a launch on Sun, 30 Aug 2026 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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100533 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
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, 6.3 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 FALCON HEAVY R/B
1 A0533U 26200A 26242.48233197 .00000000 00000-0 00000-0 0 9994
2 A0533 33.5900 12.1142 0000800 98.1200 339.2900 16.33844466 03Epoch: 2026-08-30T11:34Z
TLE epoch observation values (Epoch: 2026-08-30T11:34:33.482Z)
Latitude
32.82785°
Longitude
-65.22924°
Altitude
181.678 km
Speed
7.803 km/s
True Right ascension
05h 48m 21s
True Declination
32° 39' 27"
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
19:38:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
186.39 km
Perigee altitude
185.34 km
Semi-major axis
6,564.002 km
Eccentricity
0.00008
Inclination
33.59°
RAAN
12.1142°
Arg. of periapsis
98.12°
True anomaly
339.28676°
Mean anomaly
339.29°
Eccentric anomaly
339.28838°
Mean motion
4.08122 °/min
Orbital period
88.21 mins
BSTAR
0
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Other satellites on launch #199 in the year 2026 (2026-08-30 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 HEAVY 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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