Key statistics
Satellite SL-16 R/B at a glance.
Uptime
11345
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: 101.77 minutes
Inclination: 71.0 deg
SMA: 7220.583 km
Apoapsis: 844.344 km
Periapsis: 840.553 km
RAAN: 340.2869 deg
Eccentricy: 0.0002625
Argument of periapsis: 354.8678 deg
Mean anomaly: 5.2418 deg
Mean motion: 14.14960544 rev/day
Mean motion (dot): 0.00000136 rev/day2
B* drag term: 0.000095138 1/REarth
Two-line elements (TLE)
Creation date: May 14, 2025, 5:20 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 13, 2025, 11:25 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 23088U 94023B 25133.97600044 .00000136 00000-0 95138-4 0 9993
TLE line 2: 2 23088 71.0000 340.2869 0002625 354.8678 5.2418 14.14960544603691
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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