PEGASUS DEB, 39922
Orbit data source: Space-Track
PEGASUS DEB, 39922 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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39922 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: 2 weeks ago
TLE from 2 weeks ago
0 PEGASUS DEB
1 39922U 94029AFV 26047.85196878 .00008219 00000-0 72167-3 0 9996
2 39922 81.5844 103.0316 0109701 6.6819 353.5828 14.91881401626857Epoch: 2026-02-16T20:26Z
TLE epoch observation values (Epoch: 2026-02-16T20:26:50.102Z)
Latitude
-0.00005°
Longitude
9.48246°
Altitude
519.101 km
Speed
7.645 km/s
True Right ascension
06h 52m 07s
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
22:05:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
665.549 km
Perigee altitude
512.686 km
Semi-major axis
6,967.255 km
Eccentricity
0.01097
Inclination
81.5844°
RAAN
103.0316°
Arg. of periapsis
6.6819°
True anomaly
353.44036°
Mean anomaly
353.5828°
Eccentric anomaly
353.51178°
Mean motion
3.73208 °/min
Orbital period
96.46 mins
BSTAR
0.00072167
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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 | 2026-03-04 01:55:25.919Z | 161.601° S | 2026-03-04 01:59:25.919Z | 84.155° E | 32.056° | 2026-03-04 02:02:25.919Z | 28.36° NE |
| 7 mins | 2026-03-04 13:39:25.919Z | 339.307° N | 2026-03-04 13:42:25.919Z | 256.554° W | 41.603° | 2026-03-04 13:46:25.919Z | 185.186° SSW |
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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