Key statistics
Satellite SL-16 R/B at a glance.
Uptime
14094
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: 1987-041B
Object number (NORAD): 17974
Object ID (CCSDS): 17974
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.578 minutes
Inclination: 71.0075 deg
SMA: 7211.527 km
Apoapsis: 844.116 km
Periapsis: 822.668 km
RAAN: 217.4623 deg
Eccentricy: 0.0014871
Argument of periapsis: 330.1831 deg
Mean anomaly: 140.932 deg
Mean motion: 14.17626748 rev/day
Mean motion (dot): 0.00000021 rev/day2
B* drag term: 0.000033930258 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 2:45 a.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 17974U 87041B 25346.11495054 .00000021 00000-0 33930-4 0 9992
TLE line 2: 2 17974 71.0075 217.4623 0014871 330.1831 140.9320 14.17626748995676
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 4’, on board a Zenit-2 space rocket.
The launch took place on May 13, 1987, 5:40 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 4
Agency: N/A
Status: Launch Successful
Launch date: May 13, 1987, 5:40 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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