PEGASUS R/B, 27652

Orbit data source: Space-Track

PEGASUS R/B, 27652 is space debris in LEO originally from a launch on Sat, 25 Jan 2003 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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Identifier
27652, 2003-004B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Alliant
Mission
Spacecraft
Bus & Motor
ORION 38, Unknown motor
Mass
202 kg wet, 202 kg dry
Launch date (UTC)
2003-01-25 (23 years ago)
Launch vehicle
Unknown
Launch site
Pegasus Launch, Eastern Range Air Space (ERAS)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.7 m
Radar Cross Section
2.030 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 PEGASUS R/B
1 27652U 03004B   26115.11923914  .00001376  00000-0  13805-3 0  9991
2 27652  40.0022  62.6924 0017285 100.2707 260.0034 14.94470192261398
Epoch: 2026-04-25T02:51Z
TLE epoch observation values (Epoch: 2026-04-25T02:51:42.261Z)
Latitude
-0.00002°
Longitude
166.62411°
Altitude
585.578 km
Speed
7.568 km/s
True Right ascension
04h 10m 46s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
22:23:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
598.466 km
Perigee altitude
574.389 km
Semi-major axis
6,964.565 km
Eccentricity
0.00173
Inclination
40.0022°
RAAN
62.6924°
Arg. of periapsis
100.2707°
True anomaly
259.80841°
Mean anomaly
260.0034°
Eccentric anomaly
259.9059°
Mean motion
3.73424 °/min
Orbital period
96.41 mins
BSTAR
0.00013805
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Other satellites on launch #4 in the year 2003 (2003-01-25 UTC)

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