Key statistics
Satellite SL-24 R/B at a glance.
Uptime
6060
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.7
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: 2008-049B
Object number (NORAD): 33397
Object ID (CCSDS): 33397
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 103.452 minutes
Inclination: 98.6815 deg
SMA: 7299.949 km
Apoapsis: 1169.321 km
Periapsis: 674.307 km
RAAN: 275.6503 deg
Eccentricy: 0.0339053
Argument of periapsis: 59.7599 deg
Mean anomaly: 89.8886 deg
Mean motion: 13.91948045 rev/day
Mean motion (dot): 0.00000139 rev/day2
B* drag term: 0.000087948 1/REarth
Two-line elements (TLE)
Creation date: May 5, 2025, 2:11 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 4, 2025, 9:21 p.m. UTC
TLE line 0: 0 SL-24 R/B
TLE line 1: 1 33397U 08049B 25124.88984493 .00000139 00000-0 87948-4 0 9996
TLE line 2: 2 33397 98.6815 275.6503 0339053 59.7599 89.8886 13.91948045842745
Live tracking on map
Real-time ground track for satellite SL-24 R/B.
Associated space launch
Thai Earth observation satellite
SL-24 R/B was lifted into orbit during the mission ‘Dnepr | Thaichote’, on board a Dnepr space rocket.
The launch took place on Oct. 1, 2008, 6:37 a.m. from 370/13.
For more information about the launch, click the button.
Dnepr | Thaichote
Agency: N/A
Status: Launch Successful
Launch date: Oct. 1, 2008, 6:37 a.m. UTC
Rocket: Dnepr
Launch pad: 370/13
Location: Dombarovskiy, Russian Federation
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