Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11820
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: 100.57 minutes
Inclination: 71.0119 deg
SMA: 7163.726 km
Apoapsis: 788.866 km
Periapsis: 782.316 km
RAAN: 320.9928 deg
Eccentricy: 0.0004572
Argument of periapsis: 312.1066 deg
Mean anomaly: 47.9676 deg
Mean motion: 14.31839455 rev/day
Mean motion (dot): 0.00001558 rev/day2
B* drag term: 0.00060061 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 5:46 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39715U 92093KF 25125.24070193 .00001558 00000-0 60061-3 0 9994
TLE line 2: 2 39715 71.0119 320.9928 0004572 312.1066 47.9676 14.31839455576107
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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