Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11883
Days in orbit
Revolutions
≈ 14.6
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.1
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: 1992-093DA
Object number (NORAD): 22409
Object ID (CCSDS): 22409
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 98.583 minutes
Inclination: 71.1295 deg
SMA: 7069.035 km
Apoapsis: 773.795 km
Periapsis: 608.006 km
RAAN: 214.1962 deg
Eccentricy: 0.0117264
Argument of periapsis: 179.6465 deg
Mean anomaly: 356.707 deg
Mean motion: 14.60705053 rev/day
Mean motion (dot): 0.0000055 rev/day2
B* drag term: 0.00011424 1/REarth
Two-line elements (TLE)
Creation date: July 8, 2025, 2:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 7, 2025, 8:14 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22409U 92093DA 25188.84322731 .00000550 00000-0 11424-3 0 9999
TLE line 2: 2 22409 71.1295 214.1962 0117264 179.6465 356.7070 14.60705053698437
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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