Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12080
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: 105.059 minutes
Inclination: 70.9972 deg
SMA: 7375.333 km
Apoapsis: 1156.756 km
Periapsis: 837.64 km
RAAN: 98.4563 deg
Eccentricy: 0.02163399
Argument of periapsis: 334.9358 deg
Mean anomaly: 24.1357 deg
Mean motion: 13.70661763 rev/day
Mean motion (dot): 0.0000017 rev/day2
B* drag term: 0.00020367513 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 3:07 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 1:12 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22222U 92076D 25347.55015624 .00000170 00000-0 20368-3 0 9993
TLE line 2: 2 22222 70.9972 98.4563 0216340 334.9358 24.1357 13.70661763653244
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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