PEGASUS DEB, 24529
Orbit data source: Space-Track
PEGASUS DEB, 24529 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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24529 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: 1 week ago
TLE from 1 week ago
0 PEGASUS DEB
1 24529U 94029WD 26153.27676019 .00002603 00000-0 24370-3 0 9991
2 24529 81.9728 135.5950 0105538 336.5377 86.4045 14.89530438250068Epoch: 2026-06-02T06:38Z
TLE epoch observation values (Epoch: 2026-06-02T06:38:32.080Z)
Latitude
63.10931°
Longitude
161.26516°
Altitude
606.407 km
Speed
7.564 km/s
True Right ascension
10h 06m 36s
True Declination
62° 58' 02"
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
19:01:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
670.043 km
Perigee altitude
522.827 km
Semi-major axis
6,974.572 km
Eccentricity
0.01055
Inclination
81.9728°
RAAN
135.595°
Arg. of periapsis
336.5377°
True anomaly
87.61241°
Mean anomaly
86.4045°
Eccentric anomaly
87.00836°
Mean motion
3.72621 °/min
Orbital period
96.61 mins
BSTAR
0.0002437
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-09 09:49:01.892Z | 353.617° N | 2026-06-09 09:53:01.892Z | 135.583° SSE | 44.603° | 2026-06-09 09:57:01.892Z | 170.656° S |
| 6 mins | 2026-06-09 22:17:01.892Z | 155.329° SSE | 2026-06-09 22:20:01.892Z | 73.646° E | 33.632° | 2026-06-09 22:23:01.892Z | 24.656° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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