FALCON HEAVY DEB, 54222
Orbit data source: Space-Track
FALCON HEAVY DEB, 54222 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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54222 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 19 hours ago
0 FALCON HEAVY DEB
1 54222U 22144D 25211.78191887 -.00000087 00000-0 00000-0 0 9994
2 54222 4.9025 65.4512 0003421 199.6751 160.3981 0.98856040 8475
Epoch: 2025-07-30T18:45Z
TLE epoch observation values (Epoch: 2025-07-30T18:45:57.79Z)
Latitude
-0°
Longitude
-164.6023°
Altitude
36,201.413 km
Speed
3.059 km/s
True Right ascension
04h 22m 10s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-4.87665°
Longitude
113.39911°
Altitude
36,185.414 km
Speed
3.06 km/s
Apparent Right ascension
22h 29m 19s
Apparent Declination
-10° 45' 25"
Sunlit
Visualization observer readout
Local Sidereal Time
03:07:49
Azimuth
248.509° W
Elevation
8.196°
Doppler factor
1
Orbital elements
Apogee altitude
36,203.82 km
Perigee altitude
36,174.696 km
Semi-major axis
42,567.395 km
Eccentricity
0.00034
Inclination
4.9025°
RAAN
65.4512°
Arg. of periapsis
199.6751°
True anomaly
160.41125°
Mean anomaly
160.3981°
Eccentric anomaly
160.40467°
Mean motion
0.24713 °/min
Orbital period
1,456.72 mins
BSTAR
0
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Other satellites on launch #144 in the year 2022 (2022-11-01 UTC)
FALCON HEAVY DEB 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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697 mins | 2025-07-31 18:12:35.791Z | 252.122° W | 2025-08-01 00:37:35.791Z | 257.867° W | 12.794° | 2025-08-01 05:49:35.791Z | 256.027° W |
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54222 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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