Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11900
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
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: 1993-016D
Object number (NORAD): 22576
Object ID (CCSDS): 22576
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.84 minutes
Inclination: 70.9995 deg
SMA: 7365.107 km
Apoapsis: 1133.895 km
Periapsis: 840.049 km
RAAN: 18.6644 deg
Eccentricy: 0.01994853
Argument of periapsis: 176.8471 deg
Mean anomaly: 258.5221 deg
Mean motion: 13.73517386 rev/day
Mean motion (dot): 0.00000299 rev/day2
B* drag term: 0.00031803595 1/REarth
Two-line elements (TLE)
Creation date: Oct. 23, 2025, 2:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 22, 2025, 3:57 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22576U 93016D 25295.66509441 .00000299 00000-0 31804-3 0 9998
TLE line 2: 2 22576 70.9995 18.6644 0199485 176.8471 258.5221 13.73517386632035
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 13’, on board a Zenit-2 space rocket.
The launch took place on March 26, 1993, 2:21 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 13
Agency: N/A
Status: Launch Successful
Launch date: March 26, 1993, 2:21 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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