Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11736
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: 1993-016CC
Object number (NORAD): 39902
Object ID (CCSDS): 39902
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.772 minutes
Inclination: 71.0042 deg
SMA: 7361.909 km
Apoapsis: 1123.791 km
Periapsis: 843.758 km
RAAN: 340.7829 deg
Eccentricy: 0.0190191
Argument of periapsis: 9.4718 deg
Mean anomaly: 53.3841 deg
Mean motion: 13.74412357 rev/day
Mean motion (dot): 0.00000113 rev/day2
B* drag term: 0.00014494 1/REarth
Two-line elements (TLE)
Creation date: May 11, 2025, 2:40 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 10, 2025, 10:25 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39902U 93016CC 25130.93425091 .00000113 00000-0 14494-3 0 9996
TLE line 2: 2 39902 71.0042 340.7829 0190191 9.4718 53.3841 13.74412357548112
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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