PEGASUS DEB, 39312
Orbit data source: Space-Track
PEGASUS DEB, 39312 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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39312 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: 3 weeks ago
TLE from 3 weeks ago
0 PEGASUS DEB
1 39312U 94029AEX 26040.58438563 .00009040 00000-0 11300-2 0 9996
2 39312 81.9792 145.3140 0196411 139.3112 222.2961 14.69443748670351Epoch: 2026-02-09T14:01Z
TLE epoch observation values (Epoch: 2026-02-09T14:01:30.918Z)
Latitude
-0.00001°
Longitude
155.25807°
Altitude
769.369 km
Speed
7.414 km/s
True Right ascension
09h 41m 15s
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
04:08:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
798.138 km
Perigee altitude
521.668 km
Semi-major axis
7,038.04 km
Eccentricity
0.01964
Inclination
81.9792°
RAAN
145.314°
Arg. of periapsis
139.3112°
True anomaly
220.80866°
Mean anomaly
222.2961°
Eccentric anomaly
221.54969°
Mean motion
3.67592 °/min
Orbital period
97.93 mins
BSTAR
0.00113
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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 04:38:47.270Z | 177.19° S | 2026-03-04 04:41:47.270Z | 129.335° SE | 41.77° | 2026-03-04 04:45:47.270Z | 14.148° NNE |
| 5 mins | 2026-03-04 14:53:47.270Z | 37.257° NE | 2026-03-04 14:55:47.270Z | 71.607° E | 19.197° | 2026-03-04 14:58:47.270Z | 118.349° SE |
| 5 mins | 2026-03-04 16:32:47.270Z | 311.177° NW | 2026-03-04 16:34:47.270Z | 266.09° W | 27.028° | 2026-03-04 16:37:47.270Z | 213.037° SW |
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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