Key statistics
Satellite SL-16 R/B at a glance.
Uptime
7804
Days in orbit
Revolutions
≈ 14.1
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: 2004-021B
Object number (NORAD): 28353
Object ID (CCSDS): 28353
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.797 minutes
Inclination: 71.0002 deg
SMA: 7221.898 km
Apoapsis: 849.182 km
Periapsis: 838.344 km
RAAN: 163.9859 deg
Eccentricy: 0.0007504
Argument of periapsis: 257.8582 deg
Mean anomaly: 102.17 deg
Mean motion: 14.14574193 rev/day
Mean motion (dot): -0.00000166 rev/day2
B* drag term: -0.000061638 1/REarth
Two-line elements (TLE)
Creation date: Oct. 22, 2025, 12:16 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 21, 2025, 6:55 p.m. UTC
TLE line 0: 0 SL-16 R/B
TLE line 1: 1 28353U 04021B 25294.78841517 -.00000166 00000-0 -61638-4 0 9994
TLE line 2: 2 28353 71.0002 163.9859 0007504 257.8582 102.1700 14.14574193103191
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 22’, on board a Zenit-2 space rocket.
The launch took place on June 10, 2004, 1:28 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 22
Agency: N/A
Status: Launch Successful
Launch date: June 10, 2004, 1:28 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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