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: 17 hours ago
TLE from 17 hours ago
0 PEGASUS DEB
1 24082U 94029ED 26206.32989417 .00010989 00000-0 52029-3 0 9997
2 24082 81.9117 296.3795 0042022 75.3192 285.2693 15.18414084626132Epoch: 2026-07-25T07:55Z
TLE epoch observation values (Epoch: 2026-07-25T07:55:02.856Z)
Latitude
0.00002°
Longitude
-125.42613°
Altitude
506.189 km
Speed
7.615 km/s
True Right ascension
19h 45m 31s
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
14:22:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
536.567 km
Perigee altitude
478.696 km
Semi-major axis
6,885.768 km
Eccentricity
0.0042
Inclination
81.9117°
RAAN
296.3795°
Arg. of periapsis
75.3192°
True anomaly
284.80412°
Mean anomaly
285.2693°
Eccentric anomaly
285.03678°
Mean motion
3.79852 °/min
Orbital period
94.77 mins
BSTAR
0.00052029
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-26 06:11:40.613Z | 140.745° SSE | 2026-07-26 06:13:40.613Z | 100.007° ESE | 23.078° | 2026-07-26 06:16:40.613Z | 37.552° NE |
| 6 mins | 2026-07-26 17:41:40.613Z | 1.651° NNE | 2026-07-26 17:44:40.613Z | 117.723° SE | 40.453° | 2026-07-26 17:47:40.613Z | 162.298° S |
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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