Key statistics
Satellite SL-16 R/B at a glance.
Uptime
11237
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: 70.9831 deg
SMA: 7218.662 km
Apoapsis: 840.898 km
Periapsis: 840.157 km
RAAN: 38.1717 deg
Eccentricy: 0.00005133
Argument of periapsis: 133.0131 deg
Mean anomaly: 227.1035 deg
Mean motion: 14.1552547 rev/day
Mean motion (dot): -0.00000006 rev/day2
B* drag term: 0.000021518424 1/REarth
Two-line elements (TLE)
Creation date: Aug. 29, 2025, 2:15 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 28, 2025, 8:25 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 23405U 94077B 25240.85138654 -.00000006 00000-0 21518-4 0 9992
TLE line 2: 2 23405 70.9831 38.1717 0000513 133.0131 227.1035 14.15525470588940
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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