Key statistics
Satellite PEGASUS R/B at a glance.
Uptime
9105
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
LEO
Low Earth Orbit
Inclination
68.9
Latest
Satellite identification and parameters
Extended collection of information and parameters for PEGASUS R/B.
Object identification
Identified? True
Debris? False
Object name: PEGASUS R/B
International designator: 2000-030B
Object number (NORAD): 26375
Object ID (CCSDS): 26375
Country: UNITED STATES OF AMERICA (US)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.844 minutes
Inclination: 68.9498 deg
SMA: 7224.119 km
Apoapsis: 1285.942 km
Periapsis: 406.026 km
RAAN: 348.7529 deg
Eccentricy: 0.0609013
Argument of periapsis: 189.4565 deg
Mean anomaly: 169.4653 deg
Mean motion: 14.13921969 rev/day
Mean motion (dot): 0.00003958 rev/day2
B* drag term: 0.00032679 1/REarth
Two-line elements (TLE)
Creation date: May 12, 2025, 2:31 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 11, 2025, 8:58 p.m. UTC
TLE line 0: 0 PEGASUS R/B
TLE line 1: 1 26375U 00030B 25131.87392655 .00003958 00000-0 32679-3 0 9998
TLE line 2: 2 26375 68.9498 348.7529 0609013 189.4565 169.4653 14.13921969608063
Live tracking on map
Real-time ground track for satellite PEGASUS R/B.
Associated space launch
PEGASUS R/B was lifted into orbit during the mission ‘Pegasus XL | Tri-Services Experiments Platform-5 (TSX-5)’, on board a Pegasus XL space rocket.
The launch took place on June 7, 2000, 1:19 p.m. from Vandenberg Space Force Base.
For more information about the launch, click the button.
Pegasus XL | Tri-Services Experiments Platform-5 (TSX-5)
Agency: N/A
Status: Launch Successful
Launch date: June 7, 2000, 1:19 p.m. UTC
Rocket: Pegasus XL
Launch pad: Vandenberg Space Force Base
Location: Air launch to orbit
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