Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11941
Days in orbit
Revolutions
≈ 14.4
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: 1992-093EK
Object number (NORAD): 22442
Object ID (CCSDS): 22442
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.7 minutes
Inclination: 71.1011 deg
SMA: 7122.352 km
Apoapsis: 812.977 km
Periapsis: 675.457 km
RAAN: 41.1425 deg
Eccentricy: 0.00965407
Argument of periapsis: 151.5839 deg
Mean anomaly: 209.0614 deg
Mean motion: 14.44333901 rev/day
Mean motion (dot): 0.00020532 rev/day2
B* drag term: 0.0056293196 1/REarth
Two-line elements (TLE)
Creation date: Sept. 3, 2025, 2:21 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 2, 2025, 1:49 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22442U 92093EK 25245.57583929 .00020532 00000-0 56293-2 0 9992
TLE line 2: 2 22442 71.1011 41.1425 0096541 151.5839 209.0614 14.44333901677623
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
In-orbit conjunctions
A list of the most updated potential collisions computed for object 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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