Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11821
Days in orbit
Revolutions
≈ 14.5
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.2
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: 1992-093EV
Object number (NORAD): 22456
Object ID (CCSDS): 22456
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.994 minutes
Inclination: 71.2369 deg
SMA: 7088.682 km
Apoapsis: 759.868 km
Periapsis: 661.226 km
RAAN: 317.1477 deg
Eccentricy: 0.0069577
Argument of periapsis: 281.8146 deg
Mean anomaly: 193.4815 deg
Mean motion: 14.54636713 rev/day
Mean motion (dot): 0.00011813 rev/day2
B* drag term: 0.0026826 1/REarth
Two-line elements (TLE)
Creation date: May 7, 2025, 3:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 6, 2025, 9:05 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22456U 92093EV 25126.87858622 .00011813 00000-0 26826-2 0 9994
TLE line 2: 2 22456 71.2369 317.1477 0069577 281.8146 193.4815 14.54636713655437
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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