Key statistics
Satellite SL-16 R/B at a glance.
Uptime
10693
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.8
Latest
Satellite identification and parameters
Extended collection of information and parameters for SL-16 R/B.
Object identification
Identified? True
Debris? False
Object name: SL-16 R/B
International designator: 1996-051B
Object number (NORAD): 24298
Object ID (CCSDS): 24298
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.954 minutes
Inclination: 70.7594 deg
SMA: 7229.319 km
Apoapsis: 865.206 km
Periapsis: 837.162 km
RAAN: 0.2653 deg
Eccentricy: 0.0019396
Argument of periapsis: 261.8733 deg
Mean anomaly: 98.0187 deg
Mean motion: 14.12396636 rev/day
Mean motion (dot): 0.00000036 rev/day2
B* drag term: 0.000046118549 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 6:37 a.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 24298U 96051B 25346.27615310 .00000036 00000-0 46119-4 0 9995
TLE line 2: 2 24298 70.7594 0.2653 0019396 261.8733 98.0187 14.12396636509304
Live tracking on map
Real-time ground track for satellite SL-16 R/B.
In-orbit conjunctions
A list of the most updated potential collisions computed for object SL-16 R/B.
Associated space launch
Second generation ELING satellite
SL-16 R/B was lifted into orbit during the mission ‘Zenit-2 | Tselina-2 18’, on board a Zenit-2 space rocket.
The launch took place on Sept. 4, 1996, 9:01 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 18
Agency: N/A
Status: Launch Successful
Launch date: Sept. 4, 1996, 9:01 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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