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
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: 101.804 minutes
Inclination: 71.1702 deg
SMA: 7222.228 km
Apoapsis: 916.179 km
Periapsis: 772.007 km
RAAN: 335.1637 deg
Eccentricy: 0.00998112
Argument of periapsis: 338.3672 deg
Mean anomaly: 21.3247 deg
Mean motion: 14.14477375 rev/day
Mean motion (dot): 0.00004019 rev/day2
B* drag term: 0.0020200411 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 3:07 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 10:02 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22537U 92093GX 25347.41836997 .00004019 00000-0 20200-2 0 9990
TLE line 2: 2 22537 71.1702 335.1637 0099811 338.3672 21.3247 14.14477375678178
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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