Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11943
Days in orbit
Revolutions
≈ 13.9
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: 1992-093DS
Object number (NORAD): 22425
Object ID (CCSDS): 22425
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.231 minutes
Inclination: 71.1763 deg
SMA: 7289.546 km
Apoapsis: 994.223 km
Periapsis: 828.599 km
RAAN: 64.0745 deg
Eccentricy: 0.01136037
Argument of periapsis: 302.1079 deg
Mean anomaly: 208.611 deg
Mean motion: 13.94928824 rev/day
Mean motion (dot): 0.00000315 rev/day2
B* drag term: 0.00025372555 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, 9:53 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22425U 92093DS 25248.91232678 .00000315 00000-0 25373-3 0 9999
TLE line 2: 2 22425 71.1763 64.0745 0113604 302.1079 208.6110 13.94928824658811
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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