FALCON HEAVY R/B, 54221
Orbit data source: Space-Track
FALCON HEAVY R/B, 54221 is space debris in GEO originally from a launch on Tue, 01 Nov 2022 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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54221 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
1 day 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 1 day ago
0 FALCON HEAVY R/B
1 54221U 22144C 25211.26391600 -.00000112 00000-0 00000-0 0 9990
2 54221 5.1833 65.4476 0054424 207.7406 152.0555 0.98107318 8405Epoch: 2025-07-30T06:20Z
TLE epoch observation values (Epoch: 2025-07-30T06:20:02.342Z)
Latitude
-0°
Longitude
22.38947°
Altitude
36,609.823 km
Speed
3.038 km/s
True Right ascension
04h 22m 10s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
5.12085°
Longitude
122.82149°
Altitude
36,472.283 km
Speed
3.048 km/s
Apparent Right ascension
11h 26m 14s
Apparent Declination
0° 19' 04"
Sunlit
Visualization observer readout
Local Sidereal Time
03:17:58
Azimuth
68.35° E
Elevation
-24.25°
Doppler factor
1
Orbital elements
Apogee altitude
36,638.391 km
Perigee altitude
36,172.699 km
Semi-major axis
42,783.682 km
Eccentricity
0.00544
Inclination
5.1833°
RAAN
65.4476°
Arg. of periapsis
207.7406°
True anomaly
152.34601°
Mean anomaly
152.0555°
Eccentric anomaly
152.20093°
Mean motion
0.24526 °/min
Orbital period
1,467.83 mins
BSTAR
0
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Other satellites on launch #144 in the year 2022 (2022-11-01 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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54221 neighbors
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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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