Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12042
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.9
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: 1992-093M
Object number (NORAD): 22297
Object ID (CCSDS): 22297
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.4 minutes
Inclination: 70.9457 deg
SMA: 7250.385 km
Apoapsis: 944.035 km
Periapsis: 800.465 km
RAAN: 196.2564 deg
Eccentricy: 0.00990088
Argument of periapsis: 170.3668 deg
Mean anomaly: 189.938 deg
Mean motion: 14.06245584 rev/day
Mean motion (dot): 0.00000239 rev/day2
B* drag term: 0.0001657726 1/REarth
Two-line elements (TLE)
Creation date: Dec. 13, 2025, 4:32 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 11:55 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22297U 92093M 25346.99697745 .00000239 00000-0 16577-3 0 9994
TLE line 2: 2 22297 70.9457 196.2564 0099009 170.3668 189.9380 14.06245584687218
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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