PEGASUS DEB, 24239
Orbit data source: Space-Track
PEGASUS DEB, 24239 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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24239 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: 3 days ago
TLE from 3 days ago
0 PEGASUS DEB
1 24239U 94029LN 26171.42406235 .00005447 00000-0 59003-3 0 9997
2 24239 81.5099 156.7425 0138654 196.2933 163.3801 14.81204139576748Epoch: 2026-06-20T10:10Z
TLE epoch observation values (Epoch: 2026-06-20T10:10:38.987Z)
Latitude
0.00002°
Longitude
95.44117°
Altitude
721.71 km
Speed
7.445 km/s
True Right ascension
10h 26m 58s
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
12:51:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
719.66 km
Perigee altitude
525.524 km
Semi-major axis
7,000.729 km
Eccentricity
0.01387
Inclination
81.5099°
RAAN
156.7425°
Arg. of periapsis
196.2933°
True anomaly
163.82711°
Mean anomaly
163.3801°
Eccentric anomaly
163.60434°
Mean motion
3.70534 °/min
Orbital period
97.16 mins
BSTAR
0.00059003
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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 | 2026-06-23 10:04:57.145Z | 8.958° NNE | 2026-06-23 10:08:57.145Z | 90.041° ESE | 30.368° | 2026-06-23 10:11:57.145Z | 142.787° SSE |
| 5 mins | 2026-06-23 22:37:57.145Z | 126.628° SE | 2026-06-23 22:39:57.145Z | 91.594° ESE | 23.535° | 2026-06-23 22:42:57.145Z | 43.305° NE |
| 7 mins | 2026-06-24 00:14:57.145Z | 232.696° WSW | 2026-06-24 00:17:57.145Z | 284.196° WNW | 27.137° | 2026-06-24 00:21:57.145Z | 345.834° N |
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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