Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11920
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
Latest
Satellite identification and parameters
Extended collection of information and parameters for SL-16 DEB.
Object identification
Identified? True
Debris? True
Object name: SL-16 DEB
International designator: 1992-076D
Object number (NORAD): 22222
Object ID (CCSDS): 22222
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 105.063 minutes
Inclination: 70.9974 deg
SMA: 7375.521 km
Apoapsis: 1156.807 km
Periapsis: 837.964 km
RAAN: 51.6675 deg
Eccentricy: 0.0216149
Argument of periapsis: 202.4719 deg
Mean anomaly: 156.6805 deg
Mean motion: 13.70609536 rev/day
Mean motion (dot): 0.00000017 rev/day2
B* drag term: 0.00005722 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, 1:36 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22222U 92076D 25187.06722816 .00000017 00000-0 57220-4 0 9997
TLE line 2: 2 22222 70.9974 51.6675 0216149 202.4719 156.6805 13.70609536631254
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
In-orbit conjunctions
A list of the most updated potential collisions computed for object SL-16 DEB.
Associated space launch
Second generation ELING satellite
SL-16 DEB was lifted into orbit during the mission ‘Zenit-2 | Tselina-2 11’, on board a Zenit-2 space rocket.
The launch took place on Nov. 17, 1992, 7:47 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 11
Agency: N/A
Status: Launch Successful
Launch date: Nov. 17, 1992, 7:47 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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