Key statistics
Satellite SL-16 DEB at a glance.
Uptime
13490
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: 1988-102E
Object number (NORAD): 19658
Object ID (CCSDS): 19658
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.726 minutes
Inclination: 71.0204 deg
SMA: 7359.758 km
Apoapsis: 1126.985 km
Periapsis: 836.261 km
RAAN: 197.392 deg
Eccentricy: 0.0197509
Argument of periapsis: 340.3913 deg
Mean anomaly: 92.4564 deg
Mean motion: 13.75015052 rev/day
Mean motion (dot): 0.00000242 rev/day2
B* drag term: 0.00025927004 1/REarth
Two-line elements (TLE)
Creation date: Oct. 30, 2025, 3:32 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 29, 2025, 8:42 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 19658U 88102E 25302.86316546 .00000242 00000-0 25927-3 0 9995
TLE line 2: 2 19658 71.0204 197.3920 0197509 340.3913 92.4564 13.75015052851935
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 6’, on board a Zenit-2 space rocket.
The launch took place on Nov. 23, 1988, 2:50 p.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 6
Agency: N/A
Status: Launch Successful
Launch date: Nov. 23, 1988, 2:50 p.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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