Key statistics
Satellite SL-24 R/B at a glance.
Uptime
4338
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
97.5
Latest
Satellite identification and parameters
Extended collection of information and parameters for SL-24 R/B.
Object identification
Identified? True
Debris? False
Object name: SL-24 R/B
International designator: 2013-042B
Object number (NORAD): 39228
Object ID (CCSDS): 39228
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 102.242 minutes
Inclination: 97.5496 deg
SMA: 7242.89 km
Apoapsis: 1190.978 km
Periapsis: 538.531 km
RAAN: 86.9552 deg
Eccentricy: 0.0450405
Argument of periapsis: 122.6948 deg
Mean anomaly: 241.8499 deg
Mean motion: 14.08428971 rev/day
Mean motion (dot): 0.00000062 rev/day2
B* drag term: 0.000023004 1/REarth
Two-line elements (TLE)
Creation date: July 8, 2025, 2:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 7, 2025, 4:06 p.m. UTC
TLE line 0: 0 SL-24 R/B
TLE line 1: 1 39228U 13042B 25188.67110950 .00000062 00000-0 23004-4 0 9998
TLE line 2: 2 39228 97.5496 86.9552 0450405 122.6948 241.8499 14.08428971605801
Live tracking on map
Real-time ground track for satellite SL-24 R/B.
Associated space launch
SL-24 R/B was lifted into orbit during the mission ‘Dnepr 1 | KOMPSat-5 (Arirang-5)’, on board a Dnepr space rocket.
The launch took place on Aug. 22, 2013, 2:39 p.m. from 370/13.
For more information about the launch, click the button.
Dnepr 1 | KOMPSat-5 (Arirang-5)
Agency: N/A
Status: Launch Successful
Launch date: Aug. 22, 2013, 2:39 p.m. UTC
Rocket: Dnepr
Launch pad: 370/13
Location: Dombarovskiy, Russian Federation
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