Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11936
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.2
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: 1992-093JM
Object number (NORAD): 27750
Object ID (CCSDS): 27750
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.249 minutes
Inclination: 71.1546 deg
SMA: 7148.46 km
Apoapsis: 828.346 km
Periapsis: 712.305 km
RAAN: 6.168 deg
Eccentricy: 0.0081165
Argument of periapsis: 12.3365 deg
Mean anomaly: 347.9731 deg
Mean motion: 14.36428472 rev/day
Mean motion (dot): 0.00002105 rev/day2
B* drag term: 0.00070747494 1/REarth
Two-line elements (TLE)
Creation date: Aug. 24, 2025, 6:52 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 24, 2025, 8:34 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 27750U 92093JM 25236.35738289 .00002105 00000-0 70747-3 0 9993
TLE line 2: 2 27750 71.1546 6.1680 0081165 12.3365 347.9731 14.36428472629191
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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