PEGASUS DEB, 27679
Orbit data source: Space-Track
PEGASUS DEB, 27679 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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27679 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 days ago
TLE from 2 days ago
0 PEGASUS DEB
1 27679U 94029AEJ 26066.85351212 .00003191 00000-0 70363-3 0 9998
2 27679 81.9754 115.5030 0296375 180.1454 179.9700 14.33296857252030Epoch: 2026-03-07T20:29Z
TLE epoch observation values (Epoch: 2026-03-07T20:29:03.447Z)
Latitude
-0.00003°
Longitude
2.66943°
Altitude
995.903 km
Speed
7.244 km/s
True Right ascension
07h 42m 00s
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
15:50:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
989.922 km
Perigee altitude
565.752 km
Semi-major axis
7,155.974 km
Eccentricity
0.02964
Inclination
81.9754°
RAAN
115.503°
Arg. of periapsis
180.1454°
True anomaly
179.97171°
Mean anomaly
179.97°
Eccentric anomaly
179.97086°
Mean motion
3.58542 °/min
Orbital period
100.41 mins
BSTAR
0.00070363
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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 | 2026-03-09 14:57:41.236Z | 350.581° N | 2026-03-09 15:01:41.236Z | 273.085° WNW | 44.906° | 2026-03-09 15:05:41.236Z | 174.822° S |
| 4 mins | 2026-03-10 02:15:41.236Z | 105.391° ESE | 2026-03-10 02:17:41.236Z | 84.17° E | 14.235° | 2026-03-10 02:19:41.236Z | 62.398° ENE |
| 10 mins | 2026-03-10 03:53:41.236Z | 193.828° SSW | 2026-03-10 03:58:41.236Z | 306.553° NW | 44.039° | 2026-03-10 04:03:41.236Z | 4.599° NNE |
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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