Key statistics
Satellite SL-16 R/B at a glance.
Uptime
10533
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: 101.953 minutes
Inclination: 70.7676 deg
SMA: 7229.272 km
Apoapsis: 861.527 km
Periapsis: 840.747 km
RAAN: 338.245 deg
Eccentricy: 0.0014372
Argument of periapsis: 147.484 deg
Mean anomaly: 212.7168 deg
Mean motion: 14.12410474 rev/day
Mean motion (dot): -0.00000193 rev/day2
B* drag term: -0.000077674 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 5:45 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 1:44 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 24298U 96051B 25186.57235742 -.00000193 00000-0 -77674-4 0 9993
TLE line 2: 2 24298 70.7676 338.2450 0014372 147.4840 212.7168 14.12410474486755
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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