Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11906
Days in orbit
Revolutions
≈ 14.4
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: 1993-016AJ
Object number (NORAD): 26968
Object ID (CCSDS): 26968
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 99.833 minutes
Inclination: 70.9967 deg
SMA: 7128.703 km
Apoapsis: 757.45 km
Periapsis: 743.686 km
RAAN: 52.8005 deg
Eccentricy: 0.00096538
Argument of periapsis: 250.4466 deg
Mean anomaly: 167.3227 deg
Mean motion: 14.42404089 rev/day
Mean motion (dot): 0.0000437 rev/day2
B* drag term: 0.0013341124 1/REarth
Two-line elements (TLE)
Creation date: Oct. 28, 2025, 7:11 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 28, 2025, 9:21 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 26968U 93016AJ 25301.39024310 .00004370 00000-0 13341-2 0 9991
TLE line 2: 2 26968 70.9967 52.8005 0009654 250.4466 167.3227 14.42404089695860
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 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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