Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11938
Days in orbit
Revolutions
≈ 14.1
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: 1992-093M
Object number (NORAD): 22297
Object ID (CCSDS): 22297
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.405 minutes
Inclination: 70.947 deg
SMA: 7250.617 km
Apoapsis: 945.607 km
Periapsis: 799.357 km
RAAN: 50.4995 deg
Eccentricy: 0.01008531
Argument of periapsis: 321.9614 deg
Mean anomaly: 37.441 deg
Mean motion: 14.06178054 rev/day
Mean motion (dot): 0.00000436 rev/day2
B* drag term: 0.00028084339 1/REarth
Two-line elements (TLE)
Creation date: Sept. 1, 2025, 2:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 31, 2025, 6:45 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22297U 92093M 25243.78139750 .00000436 00000-0 28084-3 0 9999
TLE line 2: 2 22297 70.9470 50.4995 0100853 321.9614 37.4410 14.06178054672703
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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