Key statistics
Satellite SL-16 R/B at a glance.
Uptime
11555
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: 1993-059B
Object number (NORAD): 22803
Object ID (CCSDS): 22803
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.611 minutes
Inclination: 70.9896 deg
SMA: 7213.08 km
Apoapsis: 848.362 km
Periapsis: 821.528 km
RAAN: 300.3584 deg
Eccentricy: 0.0018601
Argument of periapsis: 314.2428 deg
Mean anomaly: 45.7168 deg
Mean motion: 14.17169027 rev/day
Mean motion (dot): 0.00000313 rev/day2
B* drag term: 0.00017882 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 7:21 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 22803U 93059B 25125.80632524 .00000313 00000-0 17882-3 0 9992
TLE line 2: 2 22803 70.9896 300.3584 0018601 314.2428 45.7168 14.17169027635912
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 14’, on board a Zenit-2 space rocket.
The launch took place on Sept. 16, 1993, 7:36 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 14
Agency: N/A
Status: Launch Successful
Launch date: Sept. 16, 1993, 7:36 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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