Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11937
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.2
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: 1992-093GX
Object number (NORAD): 22537
Object ID (CCSDS): 22537
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.852 minutes
Inclination: 71.1675 deg
SMA: 7224.458 km
Apoapsis: 915.723 km
Periapsis: 776.923 km
RAAN: 195.8065 deg
Eccentricy: 0.00960628
Argument of periapsis: 146.6534 deg
Mean anomaly: 214.0691 deg
Mean motion: 14.1382245 rev/day
Mean motion (dot): 0.00002098 rev/day2
B* drag term: 0.001082439 1/REarth
Two-line elements (TLE)
Creation date: Aug. 30, 2025, 3:38 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 29, 2025, 7:32 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22537U 92093GX 25241.31439754 .00002098 00000-0 10824-2 0 9998
TLE line 2: 2 22537 71.1675 195.8065 0096063 146.6534 214.0691 14.13822450663171
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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