Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11824
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: 96.386 minutes
Inclination: 71.1164 deg
SMA: 6963.653 km
Apoapsis: 631.843 km
Periapsis: 539.193 km
RAAN: 232.8019 deg
Eccentricy: 0.0066524
Argument of periapsis: 305.8366 deg
Mean anomaly: 163.2391 deg
Mean motion: 14.93987897 rev/day
Mean motion (dot): 0.00006995 rev/day2
B* drag term: 0.00063418 1/REarth
Two-line elements (TLE)
Creation date: May 9, 2025, 2:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 8, 2025, 4:39 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22327U 92093Q 25128.69437088 .00006995 00000-0 63418-3 0 9996
TLE line 2: 2 22327 71.1164 232.8019 0066524 305.8366 163.2391 14.93987897702770
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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