Key statistics
Satellite SL-16 R/B at a glance.
Uptime
11789
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: 1993-016B
Object number (NORAD): 22566
Object ID (CCSDS): 22566
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.748 minutes
Inclination: 71.0084 deg
SMA: 7219.552 km
Apoapsis: 849.49 km
Periapsis: 833.345 km
RAAN: 16.1663 deg
Eccentricy: 0.0011181
Argument of periapsis: 330.7208 deg
Mean anomaly: 29.3287 deg
Mean motion: 14.15263669 rev/day
Mean motion (dot): 0.00000222 rev/day2
B* drag term: 0.00013868 1/REarth
Two-line elements (TLE)
Creation date: July 4, 2025, 6:39 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 4, 2025, 3:04 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 22566U 93016B 25185.62795784 .00000222 00000-0 13868-3 0 9994
TLE line 2: 2 22566 71.0084 16.1663 0011181 330.7208 29.3287 14.15263669667071
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 13’, on board a Zenit-2 space rocket.
The launch took place on March 26, 1993, 2:21 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 13
Agency: N/A
Status: Launch Successful
Launch date: March 26, 1993, 2:21 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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