Key statistics
Satellite PEGASUS R/B at a glance.
Uptime
7940
Days in orbit
Revolutions
≈ 14.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
73.9
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: 2003-036B
Object number (NORAD): 27859
Object ID (CCSDS): 27859
Country: UNITED STATES OF AMERICA (US)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 96.885 minutes
Inclination: 73.9255 deg
SMA: 6987.634 km
Apoapsis: 614.113 km
Periapsis: 604.885 km
RAAN: 185.907 deg
Eccentricy: 0.0006603
Argument of periapsis: 12.6948 deg
Mean anomaly: 347.4396 deg
Mean motion: 14.86303683 rev/day
Mean motion (dot): 0.00001627 rev/day2
B* drag term: 0.00018904 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 10:46 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 8, 2025, 1:45 p.m. UTC
TLE line 0: 0 PEGASUS R/B
TLE line 1: 1 27859U 03036B 25128.57348607 .00001627 00000-0 18904-3 0 9992
TLE line 2: 2 27859 73.9255 185.9070 0006603 12.6948 347.4396 14.86303683173626
Live tracking on map
Real-time ground track for satellite PEGASUS R/B.
In-orbit conjunctions
A list of the most updated potential collisions computed for object PEGASUS R/B.
Associated space launch
PEGASUS R/B was lifted into orbit during the mission ‘Pegasus XL | SCISAT-1’, on board a Pegasus XL space rocket.
The launch took place on Aug. 13, 2003, 2:09 a.m. from Vandenberg Space Force Base.
For more information about the launch, click the button.

Pegasus XL | SCISAT-1
Agency: N/A
Status: Launch Successful
Launch date: Aug. 13, 2003, 2:09 a.m. UTC
Rocket: Pegasus XL
Launch pad: Vandenberg Space Force Base
Location: Air launch to orbit
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