Key statistics
Satellite SL-16 R/B at a glance.
Uptime
11398
Days in orbit
Revolutions
≈ 14.1
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: 1994-023B
Object number (NORAD): 23088
Object ID (CCSDS): 23088
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.769 minutes
Inclination: 70.9987 deg
SMA: 7220.541 km
Apoapsis: 846.219 km
Periapsis: 838.594 km
RAAN: 227.7575 deg
Eccentricy: 0.000528
Argument of periapsis: 295.506 deg
Mean anomaly: 64.5516 deg
Mean motion: 14.14972961 rev/day
Mean motion (dot): 0.00000108 rev/day2
B* drag term: 0.000080409 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, 1:29 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 23088U 94023B 25187.56214208 .00000108 00000-0 80409-4 0 9994
TLE line 2: 2 23088 70.9987 227.7575 0005280 295.5060 64.5516 14.14972961611278
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 15’, on board a Zenit-2 space rocket.
The launch took place on April 23, 1994, 8:01 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 15
Agency: N/A
Status: Launch Successful
Launch date: April 23, 1994, 8:01 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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