Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11820
Days in orbit
Revolutions
≈ 14.6
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.8
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: 1992-093EU
Object number (NORAD): 22455
Object ID (CCSDS): 22455
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.864 minutes
Inclination: 70.8481 deg
SMA: 7082.502 km
Apoapsis: 759.086 km
Periapsis: 649.648 km
RAAN: 156.0731 deg
Eccentricy: 0.007726
Argument of periapsis: 236.2614 deg
Mean anomaly: 186.6637 deg
Mean motion: 14.5654094 rev/day
Mean motion (dot): 0.00015065 rev/day2
B* drag term: 0.0032528 1/REarth
Two-line elements (TLE)
Creation date: May 5, 2025, 2:11 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 4, 2025, 9:13 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22455U 92093EU 25124.88471191 .00015065 00000-0 32528-2 0 9993
TLE line 2: 2 22455 70.8481 156.0731 0077260 236.2614 186.6637 14.56540940656795
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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