PEGASUS R/B, 44629
Orbit data source: Space-Track
PEGASUS R/B, 44629 is space debris in LEO originally from a launch on Fri, 11 Oct 2019 UTC launched from the Pegasus Launch, Eastern Range Air Space (ERAS). 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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44629 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NGIS FSG
Mission
Spacecraft
Bus & Motor
ORION 38, Unknown motor
Mass
202 kg wet, 202 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 0.7 m
Radar Cross Section
1.381 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 PEGASUS R/B
1 44629U 19068B 26170.85193129 .00002255 00000-0 13829-3 0 9993
2 44629 26.9930 10.0135 0011337 225.6284 134.3348 15.05227209366408Epoch: 2026-06-19T20:26Z
TLE epoch observation values (Epoch: 2026-06-19T20:26:46.863Z)
Latitude
-0.00004°
Longitude
155.24319°
Altitude
554.439 km
Speed
7.584 km/s
True Right ascension
00h 40m 03s
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
21:27:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.067 km
Perigee altitude
547.346 km
Semi-major axis
6,933.344 km
Eccentricity
0.00113
Inclination
26.993°
RAAN
10.0135°
Arg. of periapsis
225.6284°
True anomaly
134.42763°
Mean anomaly
134.3348°
Eccentric anomaly
134.38122°
Mean motion
3.75949 °/min
Orbital period
95.76 mins
BSTAR
0.00013829
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Other satellites on launch #68 in the year 2019 (2019-10-11 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 R/B Visibility
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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. |
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| PEGASUS R/B is likely not visible in the next few days. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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