PEGASUS DEB, 24129
Orbit data source: Space-Track
PEGASUS DEB, 24129 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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24129 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, 0.2 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 PEGASUS DEB
1 24129U 94029GC 26119.66453035 .00004077 00000-0 10072-2 0 9993
2 24129 81.4780 205.7135 0539543 190.5665 295.6725 13.89436020493101Epoch: 2026-04-29T15:56Z
TLE epoch observation values (Epoch: 2026-04-29T15:56:55.422Z)
Latitude
58.53365°
Longitude
-85.23507°
Altitude
787.479 km
Speed
7.543 km/s
True Right ascension
00h 46m 28s
True Declination
58° 22' 51"
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
13:38:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,321.972 km
Perigee altitude
533.6 km
Semi-major axis
7,305.923 km
Eccentricity
0.05395
Inclination
81.478°
RAAN
205.7135°
Arg. of periapsis
190.5665°
True anomaly
289.94222°
Mean anomaly
295.6725°
Eccentric anomaly
292.82318°
Mean motion
3.47561 °/min
Orbital period
103.58 mins
BSTAR
0.0010072
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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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2026-04-30 06:58:51.442Z | 203.543° SW | 2026-04-30 07:06:51.442Z | 285.446° WNW | 40.462° | 2026-04-30 07:13:51.442Z | 0.735° NNE |
| 7 mins | 2026-04-30 17:53:51.442Z | 338.398° N | 2026-04-30 17:57:51.442Z | 252.977° W | 37.708° | 2026-04-30 18:00:51.442Z | 194.184° SSW |
| 11 mins | 2026-05-01 05:28:51.442Z | 147.759° SSE | 2026-05-01 05:33:51.442Z | 97.672° ESE | 31.959° | 2026-05-01 05:39:51.442Z | 29.75° NE |
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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