Key statistics
Satellite SL-16 R/B at a glance.
Uptime
11822
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: 71.0214 deg
SMA: 7219.111 km
Apoapsis: 842.996 km
Periapsis: 838.956 km
RAAN: 286.3733 deg
Eccentricy: 0.0002798
Argument of periapsis: 23.421 deg
Mean anomaly: 336.704 deg
Mean motion: 14.15393414 rev/day
Mean motion (dot): -0.00000157 rev/day2
B* drag term: -0.000056018 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, 7:14 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 22285U 92093B 25127.80181256 -.00000157 00000-0 -56018-4 0 9999
TLE line 2: 2 22285 71.0214 286.3733 0002798 23.4210 336.7040 14.15393414669870
Live tracking on map
Real-time ground track for satellite 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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