Key statistics
Satellite SL-16 R/B at a glance.
Uptime
9392
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: 71.0042 deg
SMA: 7217.75 km
Apoapsis: 850.723 km
Periapsis: 828.508 km
RAAN: 32.1834 deg
Eccentricy: 0.00153889
Argument of periapsis: 27.1345 deg
Mean anomaly: 333.0579 deg
Mean motion: 14.15793745 rev/day
Mean motion (dot): -0.00000146 rev/day2
B* drag term: -0.000049956658 1/REarth
Two-line elements (TLE)
Creation date: Oct. 21, 2025, 3:26 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 20, 2025, 4:44 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 26070U 00006B 25293.69761514 -.00000146 00000-0 -49957-4 0 9992
TLE line 2: 2 26070 71.0042 32.1834 0015389 27.1345 333.0579 14.15793745328740
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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