Key statistics
Satellite SL-16 R/B at a glance.
Uptime
11183
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: 1994-077B
Object number (NORAD): 23405
Object ID (CCSDS): 23405
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.729 minutes
Inclination: 70.982 deg
SMA: 7218.675 km
Apoapsis: 843.008 km
Periapsis: 838.072 km
RAAN: 152.9375 deg
Eccentricy: 0.0003419
Argument of periapsis: 220.1347 deg
Mean anomaly: 139.9524 deg
Mean motion: 14.1552171 rev/day
Mean motion (dot): 0.00000265 rev/day2
B* drag term: 0.00015995 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 5:45 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 7:07 a.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 23405U 94077B 25186.29703994 .00000265 00000-0 15995-3 0 9991
TLE line 2: 2 23405 70.9820 152.9375 0003419 220.1347 139.9524 14.15521710581228
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 16’, on board a Zenit-2 space rocket.
The launch took place on Nov. 24, 1994, 9:15 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 16
Agency: N/A
Status: Launch Successful
Launch date: Nov. 24, 1994, 9:15 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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