Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12041
Days in orbit
Revolutions
≈ 14.1
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: 1992-093HW
Object number (NORAD): 22574
Object ID (CCSDS): 22574
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.778 minutes
Inclination: 71.0854 deg
SMA: 7220.984 km
Apoapsis: 931.263 km
Periapsis: 754.434 km
RAAN: 249.7479 deg
Eccentricy: 0.0122441
Argument of periapsis: 61.4511 deg
Mean anomaly: 90.6961 deg
Mean motion: 14.14842871 rev/day
Mean motion (dot): 0.00003477 rev/day2
B* drag term: 0.0016967851 1/REarth
Two-line elements (TLE)
Creation date: Dec. 11, 2025, 10:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 11, 2025, 4:41 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22574U 92093HW 25345.19540069 .00003477 00000-0 16968-2 0 9999
TLE line 2: 2 22574 71.0854 249.7479 0122441 61.4511 90.6961 14.14842871674571
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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