Key statistics
Satellite SL-16 R/B at a glance.
Uptime
11974
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: 101.636 minutes
Inclination: 70.9979 deg
SMA: 7214.276 km
Apoapsis: 844.824 km
Periapsis: 827.459 km
RAAN: 232.6682 deg
Eccentricy: 0.00120351
Argument of periapsis: 17.7415 deg
Mean anomaly: 154.9243 deg
Mean motion: 14.16816483 rev/day
Mean motion (dot): 0.00000256 rev/day2
B* drag term: 0.00015150035 1/REarth
Two-line elements (TLE)
Creation date: Aug. 30, 2025, 3:38 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 29, 2025, 6:07 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 22220U 92076B 25241.75498105 .00000256 00000-0 15150-3 0 9993
TLE line 2: 2 22220 70.9979 232.6682 0012035 17.7415 154.9243 14.16816483694645
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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