PEGASUS R/B(2), 25484

Orbit data source: Space-Track

PEGASUS R/B(2), 25484 is space debris in LEO originally from a launch on Wed, 23 Sep 1998 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
25484, 1998-053K
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
OSC Chandler
Mission
Spacecraft
Bus & Motor
HAPS, Unknown motor
Mass
97 kg wet, 97 kg dry
Launch date (UTC)
1998-09-23 (27 years ago)
Launch vehicle
Unknown
Launch site
Pegasus Launch, Eastern Range Air Space (ERAS)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.5 m
Radar Cross Section
0.355 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago
0 PEGASUS R/B(2)
1 25484U 98053K   25348.80300862  .00000333  00000-0  13650-3 0  9994
2 25484  44.5316 359.4490 0064420 253.1239 277.3890 14.43397321433938
Epoch: 2025-12-14T19:16Z
TLE epoch observation values (Epoch: 2025-12-14T19:16:19.944Z)
Latitude
7.13083°
Longitude
159.38869°
Altitude
740.99 km
Speed
7.489 km/s
True Right ascension
11h 28m 43s
True Declination
7° 05' 19"
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
13:24:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
794.834 km
Perigee altitude
703.009 km
Semi-major axis
7,127.058 km
Eccentricity
0.00644
Inclination
44.5316°
RAAN
359.449°
Arg. of periapsis
253.1239°
True anomaly
276.65619°
Mean anomaly
277.389°
Eccentric anomaly
277.02267°
Mean motion
3.60726 °/min
Orbital period
99.8 mins
BSTAR
0.0001365
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