PEGASUS DEB, 24978 (Decayed)
Orbit data source: Space-Track
PEGASUS DEB, 24978 was 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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24978 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Decayed 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
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 PEGASUS DEB
1 24978U 94029ACL 25100.03702345 .03510317 16487-1 66696-2 0 9998
2 24978 81.4001 319.2285 0028109 262.7507 97.0573 16.02876605492462Epoch: 2025-04-10T00:53Z
TLE epoch observation values (Epoch: 2025-04-10T00:53:18.826Z)
Latitude
-0.00005°
Longitude
107.3849°
Altitude
271.968 km
Speed
7.743 km/s
True Right ascension
21h 16m 54s
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
00:09:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
282.039 km
Perigee altitude
244.702 km
Semi-major axis
6,641.507 km
Eccentricity
0.00281
Inclination
81.4001°
RAAN
319.2285°
Arg. of periapsis
262.7507°
True anomaly
97.37683°
Mean anomaly
97.0573°
Eccentric anomaly
97.21708°
Mean motion
4.00999 °/min
Orbital period
89.78 mins
BSTAR
0.0066696
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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
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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