Key statistics
Satellite SL-16 R/B at a glance.
Uptime
11732
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: 101.749 minutes
Inclination: 71.004 deg
SMA: 7219.586 km
Apoapsis: 847.333 km
Periapsis: 835.57 km
RAAN: 137.737 deg
Eccentricy: 0.0008147
Argument of periapsis: 63.1738 deg
Mean anomaly: 297.0216 deg
Mean motion: 14.15253641 rev/day
Mean motion (dot): -0.00000439 rev/day2
B* drag term: -0.00020119 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 5:47 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 22566U 93016B 25127.74134825 -.00000439 00000-0 -20119-3 0 9995
TLE line 2: 2 22566 71.0040 137.7370 0008147 63.1738 297.0216 14.15253641658885
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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