Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11988
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.3
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: 1992-093EM
Object number (NORAD): 22444
Object ID (CCSDS): 22444
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.27 minutes
Inclination: 71.3224 deg
SMA: 7244.213 km
Apoapsis: 924.382 km
Periapsis: 807.775 km
RAAN: 38.6244 deg
Eccentricy: 0.00804828
Argument of periapsis: 265.7417 deg
Mean anomaly: 245.9485 deg
Mean motion: 14.08043053 rev/day
Mean motion (dot): 0.00000831 rev/day2
B* drag term: 0.00049958034 1/REarth
Two-line elements (TLE)
Creation date: Oct. 21, 2025, 3:26 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 20, 2025, 5:41 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22444U 92093EM 25293.73698118 .00000831 00000-0 49958-3 0 9993
TLE line 2: 2 22444 71.3224 38.6244 0080483 265.7417 245.9485 14.08043053678678
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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