Key statistics
Satellite SL-16 DEB at a glance.
Uptime
13672
Days in orbit
Revolutions
≈ 13.8
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: 1988-039C
Object number (NORAD): 19125
Object ID (CCSDS): 19125
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.376 minutes
Inclination: 71.0299 deg
SMA: 7343.364 km
Apoapsis: 1097.412 km
Periapsis: 833.047 km
RAAN: 100.0788 deg
Eccentricy: 0.01800028
Argument of periapsis: 283.9738 deg
Mean anomaly: 74.1408 deg
Mean motion: 13.79622139 rev/day
Mean motion (dot): 0.00000139 rev/day2
B* drag term: 0.00015761301 1/REarth
Two-line elements (TLE)
Creation date: Oct. 20, 2025, 2:10 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 19, 2025, 9:40 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 19125U 88039C 25292.90331126 .00000139 00000-0 15761-3 0 9997
TLE line 2: 2 19125 71.0299 100.0788 0180003 283.9738 74.1408 13.79622139883033
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 5’, on board a Zenit-2 space rocket.
The launch took place on May 15, 1988, 9:20 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 5
Agency: N/A
Status: Launch Successful
Launch date: May 15, 1988, 9:20 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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