Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11824
Days in orbit
Revolutions
≈ 14.1
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: 1992-093AG
Object number (NORAD): 22343
Object ID (CCSDS): 22343
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 102.023 minutes
Inclination: 70.9554 deg
SMA: 7232.561 km
Apoapsis: 920.546 km
Periapsis: 788.307 km
RAAN: 241.3044 deg
Eccentricy: 0.0091419
Argument of periapsis: 71.595 deg
Mean anomaly: 35.3419 deg
Mean motion: 14.1144696 rev/day
Mean motion (dot): 0.00000947 rev/day2
B* drag term: 0.00052709 1/REarth
Two-line elements (TLE)
Creation date: May 10, 2025, 2:32 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 9, 2025, 5:10 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22343U 92093AG 25129.71540177 .00000947 00000-0 52709-3 0 9994
TLE line 2: 2 22343 70.9554 241.3044 0091419 71.5950 35.3419 14.11446960659264
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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