Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11996
Days in orbit
Revolutions
≈ 15.0
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: 96.189 minutes
Inclination: 71.114 deg
SMA: 6954.164 km
Apoapsis: 617.607 km
Periapsis: 534.45 km
RAAN: 183.7431 deg
Eccentricy: 0.00597895
Argument of periapsis: 3.6075 deg
Mean anomaly: 99.7662 deg
Mean motion: 14.97046822 rev/day
Mean motion (dot): 0.00011196 rev/day2
B* drag term: 0.00094102415 1/REarth
Two-line elements (TLE)
Creation date: Oct. 28, 2025, 2:18 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 27, 2025, 11:17 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22327U 92093Q 25300.97081649 .00011196 00000-0 94102-3 0 9990
TLE line 2: 2 22327 71.1140 183.7431 0059790 3.6075 99.7662 14.97046822728526
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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