PEGASUS DEB, 24227
Orbit data source: Space-Track
PEGASUS DEB, 24227 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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24227 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: 17 hours ago
TLE from 17 hours ago
0 PEGASUS DEB
1 24227U 94029LA 26120.48335921 .00002512 00000-0 30399-3 0 9994
2 24227 82.0361 128.0742 0137886 69.6448 86.0954 14.76648455594711Epoch: 2026-04-30T11:36Z
TLE epoch observation values (Epoch: 2026-04-30T11:36:02.235Z)
Latitude
22.46789°
Longitude
-87.66319°
Altitude
637.484 km
Speed
7.544 km/s
True Right ascension
20h 19m 06s
True Declination
22° 20' 41"
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
12:20:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
733.699 km
Perigee altitude
540.242 km
Semi-major axis
7,015.108 km
Eccentricity
0.01379
Inclination
82.0361°
RAAN
128.0742°
Arg. of periapsis
69.6448°
True anomaly
87.67344°
Mean anomaly
86.0954°
Eccentric anomaly
86.88426°
Mean motion
3.69396 °/min
Orbital period
97.46 mins
BSTAR
0.00030399
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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 | 2026-05-01 11:50:44.927Z | 7.604° NNE | 2026-05-01 11:54:44.927Z | 81.379° E | 33.021° | 2026-05-01 11:58:44.927Z | 148.534° SSE |
| 5 mins | 2026-05-02 00:26:44.927Z | 136.035° SSE | 2026-05-02 00:28:44.927Z | 98.232° ESE | 22.655° | 2026-05-02 00:31:44.927Z | 40.359° NE |
| 4 mins | 2026-05-02 02:05:44.927Z | 255.042° W | 2026-05-02 02:07:44.927Z | 294.687° NW | 18.809° | 2026-05-02 02:09:44.927Z | 328.789° NNW |
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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