Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12041
Days in orbit
Revolutions
≈ 14.3
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: 1992-093KF
Object number (NORAD): 39715
Object ID (CCSDS): 39715
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.527 minutes
Inclination: 71.0106 deg
SMA: 7161.707 km
Apoapsis: 787.207 km
Periapsis: 779.937 km
RAAN: 205.9459 deg
Eccentricy: 0.00050752
Argument of periapsis: 317.0335 deg
Mean anomaly: 43.04 deg
Mean motion: 14.32444967 rev/day
Mean motion (dot): 0.00001615 rev/day2
B* drag term: 0.00061451163 1/REarth
Two-line elements (TLE)
Creation date: Dec. 11, 2025, 7:14 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 11, 2025, 8:01 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39715U 92093KF 25345.33441866 .00001615 00000-0 61451-3 0 9995
TLE line 2: 2 39715 71.0106 205.9459 0005075 317.0335 43.0400 14.32444967607610
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 12’, on board a Zenit-2 space rocket.
The launch took place on Dec. 25, 1992, 5:56 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 12
Agency: N/A
Status: Launch Successful
Launch date: Dec. 25, 1992, 5:56 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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