Key statistics
Satellite SL-16 R/B at a glance.
Uptime
9340
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: 2000-006B
Object number (NORAD): 26070
Object ID (CCSDS): 26070
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.71 minutes
Inclination: 71.0025 deg
SMA: 7217.785 km
Apoapsis: 850.195 km
Periapsis: 829.105 km
RAAN: 141.0741 deg
Eccentricy: 0.00146098
Argument of periapsis: 116.9275 deg
Mean anomaly: 243.3343 deg
Mean motion: 14.15783481 rev/day
Mean motion (dot): 0.00000239 rev/day2
B* drag term: 0.00014558997 1/REarth
Two-line elements (TLE)
Creation date: Aug. 30, 2025, 3:38 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 29, 2025, 9:48 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 26070U 00006B 25241.90895835 .00000239 00000-0 14559-3 0 9993
TLE line 2: 2 26070 71.0025 141.0741 0014610 116.9275 243.3343 14.15783481321418
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 21’, on board a Zenit-2 space rocket.
The launch took place on Feb. 3, 2000, 9:26 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 21
Agency: N/A
Status: Launch Successful
Launch date: Feb. 3, 2000, 9:26 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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