Key statistics
Satellite PEGASUS R/B at a glance.
Uptime
11836
Days in orbit
Revolutions
≈ 14.6
Per day
Orbit
LEO
Low Earth Orbit
Inclination
25.0
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: 1993-009C
Object number (NORAD): 22491
Object ID (CCSDS): 22491
Country: UNITED STATES OF AMERICA (US)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 98.818 minutes
Inclination: 24.9774 deg
SMA: 7080.31 km
Apoapsis: 733.615 km
Periapsis: 670.735 km
RAAN: 106.6802 deg
Eccentricy: 0.0044405
Argument of periapsis: 336.4304 deg
Mean anomaly: 23.4175 deg
Mean motion: 14.57217366 rev/day
Mean motion (dot): 0.000008 rev/day2
B* drag term: 0.00012811 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 2:28 a.m. UTC
TLE line 0: 0 PEGASUS R/B
TLE line 1: 1 22491U 93009C 25187.10343530 .00000800 00000-0 12811-3 0 9995
TLE line 2: 2 22491 24.9774 106.6802 0044405 336.4304 23.4175 14.57217366719085
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 | Satélite de Coleta de Dados-1 (SCD-1)’, on board a Pegasus space rocket.
The launch took place on Feb. 9, 1993, 2:30 p.m. from Cape Canaveral.
For more information about the launch, click the button.
Pegasus | Satélite de Coleta de Dados-1 (SCD-1)
Agency: N/A
Status: Launch Successful
Launch date: Feb. 9, 1993, 2:30 p.m. UTC
Rocket: Pegasus
Launch pad: Cape Canaveral
Location: Air launch to orbit
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