Key statistics
Satellite SL-16 R/B at a glance.
Uptime
10787
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: 1995-058B
Object number (NORAD): 23705
Object ID (CCSDS): 23705
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.735 minutes
Inclination: 71.0197 deg
SMA: 7218.942 km
Apoapsis: 851.022 km
Periapsis: 830.592 km
RAAN: 92.3992 deg
Eccentricy: 0.001415
Argument of periapsis: 225.3569 deg
Mean anomaly: 134.6402 deg
Mean motion: 14.15443223 rev/day
Mean motion (dot): -0.00000016 rev/day2
B* drag term: 0.000016402 1/REarth
Two-line elements (TLE)
Creation date: May 12, 2025, 7:41 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 12, 2025, 1:58 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 23705U 95058B 25132.58242834 -.00000016 00000-0 16402-4 0 9998
TLE line 2: 2 23705 71.0197 92.3992 0014150 225.3569 134.6402 14.15443223525248
Live tracking on map
Real-time ground track for satellite 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 17’, on board a Zenit-2 space rocket.
The launch took place on Oct. 31, 1995, 8:19 p.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 17
Agency: N/A
Status: Launch Successful
Launch date: Oct. 31, 1995, 8:19 p.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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