Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11943
Days in orbit
Revolutions
≈ 14.5
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: 1992-093W
Object number (NORAD): 22333
Object ID (CCSDS): 22333
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 99.602 minutes
Inclination: 71.0061 deg
SMA: 7117.7 km
Apoapsis: 829.042 km
Periapsis: 650.089 km
RAAN: 345.5484 deg
Eccentricy: 0.01257095
Argument of periapsis: 306.5738 deg
Mean anomaly: 52.3883 deg
Mean motion: 14.45750053 rev/day
Mean motion (dot): 0.00000692 rev/day2
B* drag term: 0.00019209111 1/REarth
Two-line elements (TLE)
Creation date: Sept. 6, 2025, 2:09 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 5, 2025, 4:51 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22333U 92093W 25248.70210829 .00000692 00000-0 19209-3 0 9997
TLE line 2: 2 22333 71.0061 345.5484 0125709 306.5738 52.3883 14.45750053698948
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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