PEGASUS R/B, 25281
Orbit data source: Space-Track
PEGASUS R/B, 25281 is space debris in SSO originally from a launch on Thu, 02 Apr 1998 UTC launched from the Pegasus Launch, Western Range Air Space (WRAS). 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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25281 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
18 hours ago
Origin
Manufacturer
OSCC/ATKH
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 & history
TLE from 18 hours ago
0 PEGASUS R/B
1 25281U 98020B 25199.68496240 .00038603 00000-0 40243-3 0 9998
2 25281 97.3482 61.8310 0003395 192.1552 167.9626 15.64441831501603Epoch: 2025-07-18T16:26Z
TLE epoch observation values (Epoch: 2025-07-18T16:26:20.751Z)
Latitude
-0.00001°
Longitude
-121.48834°
Altitude
380.239 km
Speed
7.68 km/s
True Right ascension
04h 07m 19s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-65.66671°
Longitude
42.81639°
Altitude
398.42 km
Speed
7.671 km/s
Apparent Right ascension
12h 33m 45s
Apparent Declination
-56° 20' 55"
Sunlit
Visualization observer readout
Local Sidereal Time
23:11:56
Azimuth
212.385° SW
Elevation
-68.805°
Doppler factor
1
Orbital elements
Apogee altitude
374.04 km
Perigee altitude
369.457 km
Semi-major axis
6,749.886 km
Eccentricity
0.00034
Inclination
97.3482°
RAAN
61.831°
Arg. of periapsis
192.1552°
True anomaly
167.97071°
Mean anomaly
167.9626°
Eccentric anomaly
167.96666°
Mean motion
3.9138 °/min
Orbital period
91.98 mins
BSTAR
0.00040243
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Other satellites on launch #20 in the year 1998 (1998-04-02 UTC)
PEGASUS R/B Visibility
Observer location: undefined°, undefined°
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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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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Authenticating...
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