PEGASUS DEB, 24082
Orbit data source: Space-Track
PEGASUS DEB, 24082 is 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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24082 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 PEGASUS DEB
1 24082U 94029ED 26062.46870186 .00011562 00000-0 59609-3 0 9993
2 24082 81.9089 89.8547 0043330 203.2720 156.6551 15.15413352604327Epoch: 2026-03-03T11:14Z
TLE epoch observation values (Epoch: 2026-03-03T11:14:55.840Z)
Latitude
-0°
Longitude
119.87471°
Altitude
550.255 km
Speed
7.572 km/s
True Right ascension
05h 59m 25s
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
22:04:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
546.602 km
Perigee altitude
486.851 km
Semi-major axis
6,894.863 km
Eccentricity
0.00433
Inclination
81.9089°
RAAN
89.8547°
Arg. of periapsis
203.272°
True anomaly
156.85088°
Mean anomaly
156.6551°
Eccentric anomaly
156.75309°
Mean motion
3.79101 °/min
Orbital period
94.96 mins
BSTAR
0.00059609
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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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-04 01:39:24.397Z | 121.609° SE | 2026-03-04 01:41:24.397Z | 85.511° E | 17.557° | 2026-03-04 01:43:24.397Z | 51.489° ENE |
| 4 mins | 2026-03-04 03:15:24.397Z | 247.764° W | 2026-03-04 03:16:24.397Z | 270.938° WNW | 24.922° | 2026-03-04 03:19:24.397Z | 336.352° NNW |
| 5 mins | 2026-03-04 13:11:24.397Z | 26.047° NE | 2026-03-04 13:13:24.397Z | 94.596° ESE | 31.877° | 2026-03-04 13:16:24.397Z | 148.18° SSE |
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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