Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11851
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: 99.931 minutes
Inclination: 71.1253 deg
SMA: 7133.348 km
Apoapsis: 819.365 km
Periapsis: 691.062 km
RAAN: 132.0774 deg
Eccentricy: 0.0089932
Argument of periapsis: 337.0494 deg
Mean anomaly: 22.6634 deg
Mean motion: 14.4099552 rev/day
Mean motion (dot): 0.00022016 rev/day2
B* drag term: 0.0065189174 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, 11 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 42239U 93016CT 25243.95853218 .00022016 00000-0 65189-2 0 9998
TLE line 2: 2 42239 71.1253 132.0774 0089932 337.0494 22.6634 14.40995520892737
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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