Key statistics
Satellite SL-16 R/B at a glance.
Uptime
13670
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: 1988-039B
Object number (NORAD): 19120
Object ID (CCSDS): 19120
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.438 minutes
Inclination: 71.0173 deg
SMA: 7204.901 km
Apoapsis: 843.185 km
Periapsis: 810.348 km
RAAN: 13.3638 deg
Eccentricy: 0.00227878
Argument of periapsis: 206.7997 deg
Mean anomaly: 153.1952 deg
Mean motion: 14.19582752 rev/day
Mean motion (dot): -0.00000035 rev/day2
B* drag term: 0.00000617856 1/REarth
Two-line elements (TLE)
Creation date: Oct. 16, 2025, 6:34 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 16, 2025, 12:43 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 19120U 88039B 25289.53011398 -.00000035 00000-0 61786-5 0 9999
TLE line 2: 2 19120 71.0173 13.3638 0022788 206.7997 153.1952 14.19582752937925
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 5’, on board a Zenit-2 space rocket.
The launch took place on May 15, 1988, 9:20 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 5
Agency: N/A
Status: Launch Successful
Launch date: May 15, 1988, 9:20 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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