Key statistics
Satellite SL-16 R/B at a glance.
Uptime
11342
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: 101.727 minutes
Inclination: 70.9812 deg
SMA: 7218.581 km
Apoapsis: 843.807 km
Periapsis: 837.085 km
RAAN: 176.3717 deg
Eccentricy: 0.0004656
Argument of periapsis: 284.4905 deg
Mean anomaly: 75.5701 deg
Mean motion: 14.1554947 rev/day
Mean motion (dot): 0.00000317 rev/day2
B* drag term: 0.00018648482 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, 6:49 a.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 23405U 94077B 25346.28436988 .00000317 00000-0 18648-3 0 9990
TLE line 2: 2 23405 70.9812 176.3717 0004656 284.4905 75.5701 14.15549470603866
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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