PEGASUS DEB, 39308
Orbit data source: Space-Track
PEGASUS DEB, 39308 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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39308 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
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 PEGASUS DEB
1 39308U 94029AET 26111.62285711 .00002441 00000-0 44754-3 0 9998
2 39308 81.9644 74.6281 0340410 195.3301 163.7376 14.34195732672613Epoch: 2026-04-21T14:56Z
TLE epoch observation values (Epoch: 2026-04-21T14:56:54.854Z)
Latitude
0.00001°
Longitude
0.70356°
Altitude
1,015.211 km
Speed
7.223 km/s
True Right ascension
04h 58m 30s
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
15:38:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,018.338 km
Perigee altitude
531.349 km
Semi-major axis
7,152.981 km
Eccentricity
0.03404
Inclination
81.9644°
RAAN
74.6281°
Arg. of periapsis
195.3301°
True anomaly
164.78698°
Mean anomaly
163.7376°
Eccentric anomaly
164.26648°
Mean motion
3.58767 °/min
Orbital period
100.34 mins
BSTAR
0.00044754
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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 | 2026-04-22 09:58:04.655Z | 334.41° NNW | 2026-04-22 10:02:04.655Z | 273.171° WNW | 29.998° | 2026-04-22 10:05:04.655Z | 210.33° SW |
| 9 mins | 2026-04-22 21:13:04.655Z | 137.815° SSE | 2026-04-22 21:17:04.655Z | 89.208° E | 26.399° | 2026-04-22 21:22:04.655Z | 32.167° NE |
| 10 mins | 2026-04-22 22:53:04.655Z | 216.768° SW | 2026-04-22 22:58:04.655Z | 280.463° WNW | 34.323° | 2026-04-22 23:03:04.655Z | 350.351° 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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