Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11946
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.9
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: 1992-093KN
Object number (NORAD): 39722
Object ID (CCSDS): 39722
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.73 minutes
Inclination: 70.8916 deg
SMA: 7265.934 km
Apoapsis: 965.265 km
Periapsis: 810.332 km
RAAN: 243.2268 deg
Eccentricy: 0.01066164
Argument of periapsis: 322.1504 deg
Mean anomaly: 48.5746 deg
Mean motion: 14.01734079 rev/day
Mean motion (dot): 0.0000094 rev/day2
B* drag term: 0.00061887268 1/REarth
Two-line elements (TLE)
Creation date: Sept. 6, 2025, 10:23 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 6, 2025, 5:48 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39722U 92093KN 25249.24176427 .00000940 00000-0 61887-3 0 9997
TLE line 2: 2 39722 70.8916 243.2268 0106616 322.1504 48.5746 14.01734079581857
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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