Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12042
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.8
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: 1992-093BQ
Object number (NORAD): 22375
Object ID (CCSDS): 22375
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 102.747 minutes
Inclination: 70.8139 deg
SMA: 7266.727 km
Apoapsis: 954.489 km
Periapsis: 822.695 km
RAAN: 173.6213 deg
Eccentricy: 0.0090683
Argument of periapsis: 323.75 deg
Mean anomaly: 186.1763 deg
Mean motion: 14.01504502 rev/day
Mean motion (dot): 0.00000197 rev/day2
B* drag term: 0.00015616 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 7:26 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 11, 2025, 10:53 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22375U 92093BQ 25345.95371336 .00000197 00000-0 15616-3 0 9997
TLE line 2: 2 22375 70.8139 173.6213 0090683 323.7500 186.1763 14.01504502682839
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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