Key statistics
Satellite SL-24 R/B at a glance.
Uptime
6094
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.0
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: 2008-040H
Object number (NORAD): 33319
Object ID (CCSDS): 33319
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 104.675 minutes
Inclination: 97.9834 deg
SMA: 7357.348 km
Apoapsis: 1343.258 km
Periapsis: 615.167 km
RAAN: 32.513 deg
Eccentricy: 0.0494805
Argument of periapsis: 47.9802 deg
Mean anomaly: 10.7567 deg
Mean motion: 13.75690834 rev/day
Mean motion (dot): 0.00000236 rev/day2
B* drag term: 0.000114 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 6:24 p.m. UTC
TLE line 0: 0 SL-24 R/B
TLE line 1: 1 33319U 08040H 25125.76693771 .00000236 00000-0 11400-3 0 9992
TLE line 2: 2 33319 97.9834 32.5130 0494805 47.9802 10.7567 13.75690834837296
Live tracking on map
Real-time ground track for satellite SL-24 R/B.
Associated space launch
German Earth observation satellites
SL-24 R/B was lifted into orbit during the mission ‘Dnepr | RapidEye 1 to 5’, on board a Dnepr space rocket.
The launch took place on Aug. 29, 2008, 7:15 a.m. from 109/95.
For more information about the launch, click the button.
Dnepr | RapidEye 1 to 5
Agency: N/A
Status: Launch Successful
Launch date: Aug. 29, 2008, 7:15 a.m. UTC
Rocket: Dnepr
Launch pad: 109/95
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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