PEGASUS DEB, 24165 (Decayed)
Orbit data source: Space-Track
PEGASUS DEB, 24165 was space debris in LEO originally from a launch on Thu, 19 May 1994 UTC launched from the Air Force Western Test Range (AFWTR). 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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24165 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 PEGASUS DEB
1 24165U 94029HQ 26025.65018758 .05018022 58284-1 10064-1 0 9995
2 24165 82.1187 276.9331 0017284 110.9004 249.4127 16.05140621539557Epoch: 2026-01-25T15:36Z
TLE epoch observation values (Epoch: 2026-01-25T15:36:16.206Z)
Latitude
-0.00013°
Longitude
-82.09169°
Altitude
267.451 km
Speed
7.744 km/s
True Right ascension
18h 27m 43s
True Declination
0° 00' 00"
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
18:33:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
268.551 km
Perigee altitude
245.614 km
Semi-major axis
6,635.22 km
Eccentricity
0.00173
Inclination
82.1187°
RAAN
276.9331°
Arg. of periapsis
110.9004°
True anomaly
249.22743°
Mean anomaly
249.4127°
Eccentric anomaly
249.32005°
Mean motion
4.01569 °/min
Orbital period
89.65 mins
BSTAR
0.010064
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Other satellites on launch #29 in the year 1994 (1994-05-19 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.PEGASUS DEB 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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