Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11854
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: 104.842 minutes
Inclination: 70.9953 deg
SMA: 7365.19 km
Apoapsis: 1135.373 km
Periapsis: 838.738 km
RAAN: 106.495 deg
Eccentricy: 0.02013759
Argument of periapsis: 239.9822 deg
Mean anomaly: 215.3743 deg
Mean motion: 13.73494084 rev/day
Mean motion (dot): 0.00000071 rev/day2
B* drag term: 0.00010632771 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 3:16 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 7, 2025, 9:07 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22576U 93016D 25250.88029154 .00000071 00000-0 10633-3 0 9996
TLE line 2: 2 22576 70.9953 106.4950 0201376 239.9822 215.3743 13.73494084625883
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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