Key statistics
Satellite SL-16 R/B at a glance.
Uptime
11882
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: 1992-093B
Object number (NORAD): 22285
Object ID (CCSDS): 22285
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.738 minutes
Inclination: 71.0209 deg
SMA: 7219.081 km
Apoapsis: 845.251 km
Periapsis: 836.642 km
RAAN: 161.3174 deg
Eccentricy: 0.0005963
Argument of periapsis: 305.714 deg
Mean anomaly: 54.3428 deg
Mean motion: 14.15402156 rev/day
Mean motion (dot): 0.00000121 rev/day2
B* drag term: 0.000086525 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 9:05 a.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 22285U 92093B 25187.37894583 .00000121 00000-0 86525-4 0 9996
TLE line 2: 2 22285 71.0209 161.3174 0005963 305.7140 54.3428 14.15402156678305
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 12’, on board a Zenit-2 space rocket.
The launch took place on Dec. 25, 1992, 5:56 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 12
Agency: N/A
Status: Launch Successful
Launch date: Dec. 25, 1992, 5:56 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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