Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11738
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.1
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: 1993-016CT
Object number (NORAD): 42239
Object ID (CCSDS): 42239
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.084 minutes
Inclination: 71.1288 deg
SMA: 7140.611 km
Apoapsis: 830.998 km
Periapsis: 693.954 km
RAAN: 13.3538 deg
Eccentricy: 0.0095961
Argument of periapsis: 155.9998 deg
Mean anomaly: 204.5657 deg
Mean motion: 14.38797715 rev/day
Mean motion (dot): 0.00008124 rev/day2
B* drag term: 0.0025158 1/REarth
Two-line elements (TLE)
Creation date: May 14, 2025, 6:56 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 12, 2025, 10:26 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 42239U 93016CT 25132.93512617 .00008124 00000-0 25158-2 0 9994
TLE line 2: 2 42239 71.1288 13.3538 0095961 155.9998 204.5657 14.38797715876752
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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