Key statistics
Satellite SL-16 R/B at a glance.
Uptime
11557
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: 1994-023B
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: 101.767 minutes
Inclination: 71.0008 deg
SMA: 7220.439 km
Apoapsis: 843.269 km
Periapsis: 841.339 km
RAAN: 254.6235 deg
Eccentricy: 0.00013366
Argument of periapsis: 27.8994 deg
Mean anomaly: 332.22 deg
Mean motion: 14.15002954 rev/day
Mean motion (dot): 0.00000054 rev/day2
B* drag term: 0.000052699293 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, 4:45 a.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 23088U 94023B 25346.19797096 .00000054 00000-0 52699-4 0 9991
TLE line 2: 2 23088 71.0008 254.6235 0001337 27.8994 332.2200 14.15002954633712
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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