Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12042
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.7
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: 1992-093JB
Object number (NORAD): 22812
Object ID (CCSDS): 22812
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.278 minutes
Inclination: 70.6858 deg
SMA: 7244.596 km
Apoapsis: 961.085 km
Periapsis: 771.838 km
RAAN: 332.9341 deg
Eccentricy: 0.01306121
Argument of periapsis: 311.7189 deg
Mean anomaly: 47.2813 deg
Mean motion: 14.07931319 rev/day
Mean motion (dot): 0.00004444 rev/day2
B* drag term: 0.0024451839 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 3:07 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 8:03 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22812U 92093JB 25347.33590680 .00004444 00000-0 24452-2 0 9998
TLE line 2: 2 22812 70.6858 332.9341 0130612 311.7189 47.2813 14.07931319656841
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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