PEGASUS DEB, 24126
Orbit data source: Space-Track
PEGASUS DEB, 24126 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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24126 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: 8 hours ago
TLE from 8 hours ago
0 PEGASUS DEB
1 24126U 94029FZ 26227.61415021 .00001795 00000-0 34370-3 0 9990
2 24126 81.7986 285.6959 0267063 350.6487 171.6248 14.43028874562538Epoch: 2026-08-15T14:44Z
TLE epoch observation values (Epoch: 2026-08-15T14:44:22.578Z)
Latitude
17.09861°
Longitude
-81.94855°
Altitude
939.295 km
Speed
7.285 km/s
True Right ascension
06h 52m 40s
True Declination
17° 00' 17"
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
12:58:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
935.858 km
Perigee altitude
555.361 km
Semi-major axis
7,123.746 km
Eccentricity
0.02671
Inclination
81.7986°
RAAN
285.6959°
Arg. of periapsis
350.6487°
True anomaly
172.05628°
Mean anomaly
171.6248°
Eccentric anomaly
171.84194°
Mean motion
3.60978 °/min
Orbital period
99.73 mins
BSTAR
0.0003437
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-16 05:05:45.684Z | 207.862° SW | 2026-08-16 05:08:45.684Z | 283.875° WNW | 39.43° | 2026-08-16 05:12:45.684Z | 358.586° N |
| 10 mins | 2026-08-16 15:30:45.684Z | 359.925° N | 2026-08-16 15:35:45.684Z | 108.94° ESE | 41.935° | 2026-08-16 15:40:45.684Z | 161.7° S |
| 5 mins | 2026-08-16 17:13:45.684Z | 294.536° NW | 2026-08-16 17:15:45.684Z | 270.625° WNW | 16.449° | 2026-08-16 17:18:45.684Z | 239.495° WSW |
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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