Key statistics
Satellite SL-16 R/B at a glance.
Uptime
11920
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
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: 1992-076B
Object number (NORAD): 22220
Object ID (CCSDS): 22220
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.637 minutes
Inclination: 71.0009 deg
SMA: 7214.306 km
Apoapsis: 843.995 km
Periapsis: 828.348 km
RAAN: 346.7733 deg
Eccentricy: 0.0010844
Argument of periapsis: 114.4094 deg
Mean anomaly: 314.2102 deg
Mean motion: 14.16807608 rev/day
Mean motion (dot): -0.00000058 rev/day2
B* drag term: -0.0000051848 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 2:46 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 1:59 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 22220U 92076B 25187.58277826 -.00000058 00000-0 -51848-5 0 9996
TLE line 2: 2 22220 71.0009 346.7733 0010844 114.4094 314.2102 14.16807608687308
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 11’, on board a Zenit-2 space rocket.
The launch took place on Nov. 17, 1992, 7:47 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 11
Agency: N/A
Status: Launch Successful
Launch date: Nov. 17, 1992, 7:47 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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