Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11938
Days in orbit
Revolutions
≈ 14.1
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: 1992-093DH
Object number (NORAD): 22416
Object ID (CCSDS): 22416
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.406 minutes
Inclination: 70.961 deg
SMA: 7250.646 km
Apoapsis: 928.575 km
Periapsis: 816.446 km
RAAN: 24.5146 deg
Eccentricy: 0.00773229
Argument of periapsis: 63.1107 deg
Mean anomaly: 62.7096 deg
Mean motion: 14.06169752 rev/day
Mean motion (dot): 0.0000007 rev/day2
B* drag term: 0.000068854297 1/REarth
Two-line elements (TLE)
Creation date: Sept. 1, 2025, 2:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 31, 2025, 8:29 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22416U 92093DH 25243.85414395 .00000070 00000-0 68854-4 0 9995
TLE line 2: 2 22416 70.9610 24.5146 0077323 63.1107 62.7096 14.06169752674954
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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