PEGASUS DEB, 39319
Orbit data source: Space-Track
PEGASUS DEB, 39319 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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39319 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: 1 day ago
TLE from 1 day ago
0 PEGASUS DEB
1 39319U 94029AFE 26061.96119359 .00001954 00000-0 26990-3 0 9995
2 39319 81.9450 144.7275 0179272 261.2632 96.8233 14.67165690262752Epoch: 2026-03-02T23:04Z
TLE epoch observation values (Epoch: 2026-03-02T23:04:07.126Z)
Latitude
0.00003°
Longitude
-2.04929°
Altitude
690.372 km
Speed
7.502 km/s
True Right ascension
09h 38m 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
07:58:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
793.497 km
Perigee altitude
540.891 km
Semi-major axis
7,045.331 km
Eccentricity
0.01793
Inclination
81.945°
RAAN
144.7275°
Arg. of periapsis
261.2632°
True anomaly
98.85721°
Mean anomaly
96.8233°
Eccentric anomaly
97.84085°
Mean motion
3.67021 °/min
Orbital period
98.09 mins
BSTAR
0.0002699
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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 | 2026-03-04 06:18:08.297Z | 195.864° SSW | 2026-03-04 06:21:08.297Z | 255.928° W | 44.01° | 2026-03-04 06:26:08.297Z | 4.648° NNE |
| 7 mins | 2026-03-04 16:35:08.297Z | 19.752° NNE | 2026-03-04 16:38:08.297Z | 79.212° E | 31.506° | 2026-03-04 16:42:08.297Z | 141.922° SSE |
| 6 mins | 2026-03-04 18:14:08.297Z | 311.196° NW | 2026-03-04 18:17:08.297Z | 265.815° W | 19.987° | 2026-03-04 18:20:08.297Z | 226.139° WSW |
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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