PEGASUS DEB, 39932
Orbit data source: Space-Track
PEGASUS DEB, 39932 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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39932 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: 4 days ago
TLE from 4 days ago
0 PEGASUS DEB
1 39932U 94029AGF 26045.11014376 .00001717 00000-0 40365-3 0 9997
2 39932 81.8195 327.3347 0298478 117.0192 246.1796 14.29997731606850Epoch: 2026-02-14T02:38Z
TLE epoch observation values (Epoch: 2026-02-14T02:38:36.420Z)
Latitude
-0.00009°
Longitude
143.54503°
Altitude
886.387 km
Speed
7.362 km/s
True Right ascension
21h 49m 20s
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
05:14:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,002.774 km
Perigee altitude
574.936 km
Semi-major axis
7,166.992 km
Eccentricity
0.02985
Inclination
81.8195°
RAAN
327.3347°
Arg. of periapsis
117.0192°
True anomaly
243.09861°
Mean anomaly
246.1796°
Eccentric anomaly
244.63432°
Mean motion
3.57716 °/min
Orbital period
100.64 mins
BSTAR
0.00040365
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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 | 2026-02-18 06:17:22.091Z | 347.022° N | 2026-02-18 06:21:22.091Z | 216.101° SW | 42.829° | 2026-02-18 06:25:22.091Z | 178.746° S |
| 7 mins | 2026-02-18 19:17:22.091Z | 203.572° SW | 2026-02-18 19:20:22.091Z | 256.992° W | 40.653° | 2026-02-18 19:24:22.091Z | 358.437° 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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