Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11823
Days in orbit
Revolutions
≈ 14.2
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: 1992-093CD
Object number (NORAD): 22388
Object ID (CCSDS): 22388
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.647 minutes
Inclination: 70.9651 deg
SMA: 7214.789 km
Apoapsis: 908.901 km
Periapsis: 764.408 km
RAAN: 326.2529 deg
Eccentricy: 0.0100137
Argument of periapsis: 148.1554 deg
Mean anomaly: 328.4373 deg
Mean motion: 14.16665338 rev/day
Mean motion (dot): 0.00002823 rev/day2
B* drag term: 0.0013676 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 10:36 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 8, 2025, 3:58 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22388U 92093CD 25128.66539134 .00002823 00000-0 13676-2 0 9991
TLE line 2: 2 22388 70.9651 326.2529 0100137 148.1554 328.4373 14.16665338655360
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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