Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11820
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.7
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: 1992-093P
Object number (NORAD): 22326
Object ID (CCSDS): 22326
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.026 minutes
Inclination: 70.6616 deg
SMA: 7279.866 km
Apoapsis: 1002.375 km
Periapsis: 801.087 km
RAAN: 219.7527 deg
Eccentricy: 0.013825
Argument of periapsis: 108.4329 deg
Mean anomaly: 317.6892 deg
Mean motion: 13.97712046 rev/day
Mean motion (dot): 0.00001584 rev/day2
B* drag term: 0.0010644 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 8:31 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22326U 92093P 25125.35510404 .00001584 00000-0 10644-2 0 9990
TLE line 2: 2 22326 70.6616 219.7527 0138250 108.4329 317.6892 13.97712046637475
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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