Key statistics
Satellite SL-16 R/B at a glance.
Uptime
9286
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: 101.711 minutes
Inclination: 71.0018 deg
SMA: 7217.798 km
Apoapsis: 852.159 km
Periapsis: 827.167 km
RAAN: 255.3056 deg
Eccentricy: 0.0017313
Argument of periapsis: 203.1783 deg
Mean anomaly: 156.8561 deg
Mean motion: 14.15779691 rev/day
Mean motion (dot): 0.00000248 rev/day2
B* drag term: 0.0001502 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 1:50 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 26070U 00006B 25187.57640174 .00000248 00000-0 15020-3 0 9993
TLE line 2: 2 26070 71.0018 255.3056 0017313 203.1783 156.8561 14.15779691313727
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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