Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11883
Days in orbit
Revolutions
≈ 14.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.1
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: 1992-093Q
Object number (NORAD): 22327
Object ID (CCSDS): 22327
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 96.344 minutes
Inclination: 71.1162 deg
SMA: 6961.638 km
Apoapsis: 629.04 km
Periapsis: 537.967 km
RAAN: 89.9369 deg
Eccentricy: 0.0065411
Argument of periapsis: 203.2573 deg
Mean anomaly: 270.4493 deg
Mean motion: 14.94636484 rev/day
Mean motion (dot): 0.00003982 rev/day2
B* drag term: 0.00035887 1/REarth
Two-line elements (TLE)
Creation date: July 8, 2025, 2:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 7, 2025, 10:36 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22327U 92093Q 25188.94214714 .00003982 00000-0 35887-3 0 9991
TLE line 2: 2 22327 71.1162 89.9369 0065411 203.2573 270.4493 14.94636484711770
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
Associated space launch
Second generation ELING satellite
SL-16 DEB was lifted into orbit during the mission ‘Zenit-2 | Tselina-2 12’, on board a Zenit-2 space rocket.
The launch took place on Dec. 25, 1992, 5:56 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 12
Agency: N/A
Status: Launch Successful
Launch date: Dec. 25, 1992, 5:56 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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