Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11826
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.1
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: 1992-093DB
Object number (NORAD): 22410
Object ID (CCSDS): 22410
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.069 minutes
Inclination: 71.0846 deg
SMA: 7281.926 km
Apoapsis: 983.529 km
Periapsis: 824.053 km
RAAN: 83.7969 deg
Eccentricy: 0.0109501
Argument of periapsis: 234.8692 deg
Mean anomaly: 151.8039 deg
Mean motion: 13.97118858 rev/day
Mean motion (dot): 0.00000215 rev/day2
B* drag term: 0.00017693 1/REarth
Two-line elements (TLE)
Creation date: May 12, 2025, 2:31 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 11, 2025, 8:05 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22410U 92093DB 25131.83748109 .00000215 00000-0 17693-3 0 9991
TLE line 2: 2 22410 71.0846 83.7969 0109501 234.8692 151.8039 13.97118858645765
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
In-orbit conjunctions
A list of the most updated potential collisions computed for object 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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