PEGASUS DEB, 39306
Orbit data source: Space-Track
PEGASUS DEB, 39306 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.
Focus sentinelFocus sentinel
Request partner network tasking
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
39306 intel report (Beta)
Focus sentinelFocus sentinel
Edit Public Description
Focus sentinelFocus sentinel
Create New Watchlist
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 PEGASUS DEB
1 39306U 94029AER 26057.27733312 .00074995 00000-0 46128-2 0 9990
2 39306 81.7323 356.2383 0122741 77.7128 283.7806 15.03561005 92186Epoch: 2026-02-26T06:39Z
TLE epoch observation values (Epoch: 2026-02-26T06:39:21.581Z)
Latitude
-0.00007°
Longitude
100.2679°
Altitude
539.681 km
Speed
7.603 km/s
True Right ascension
23h 44m 57s
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
14:34:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
638.025 km
Perigee altitude
467.879 km
Semi-major axis
6,931.089 km
Eccentricity
0.01227
Inclination
81.7323°
RAAN
356.2383°
Arg. of periapsis
77.7128°
True anomaly
282.4097°
Mean anomaly
283.7806°
Eccentric anomaly
283.09564°
Mean motion
3.76133 °/min
Orbital period
95.71 mins
BSTAR
0.0046128
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #29 in the year 1994 (1994-05-19 UTC)
Did you know?
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
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-07 19:04:22.139Z | 160.361° S | 2026-03-07 19:07:22.139Z | 77.598° E | 32.079° | 2026-03-07 19:09:22.139Z | 30.721° NE |
| 6 mins | 2026-03-08 06:41:22.139Z | 336.145° NNW | 2026-03-08 06:43:22.139Z | 262.634° W | 41.595° | 2026-03-08 06:47:22.139Z | 183.537° 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 |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
|---|