Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11823
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.7
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: 1992-093KH
Object number (NORAD): 39717
Object ID (CCSDS): 39717
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.663 minutes
Inclination: 70.6811 deg
SMA: 7262.769 km
Apoapsis: 959.292 km
Periapsis: 809.976 km
RAAN: 274.3374 deg
Eccentricy: 0.0102795
Argument of periapsis: 177.7626 deg
Mean anomaly: 182.397 deg
Mean motion: 14.0265029 rev/day
Mean motion (dot): 0.00001809 rev/day2
B* drag term: 0.0011484 1/REarth
Two-line elements (TLE)
Creation date: May 2, 2025, 2:33 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 1, 2025, 2:29 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39717U 92093KH 25121.10351288 .00001809 00000-0 11484-2 0 9997
TLE line 2: 2 39717 70.6811 274.3374 0102795 177.7626 182.3970 14.02650290564668
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 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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