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
71.3
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: 1992-093FP
Object number (NORAD): 22474
Object ID (CCSDS): 22474
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.791 minutes
Inclination: 71.2997 deg
SMA: 7221.616 km
Apoapsis: 944.661 km
Periapsis: 742.301 km
RAAN: 288.6599 deg
Eccentricy: 0.01401075
Argument of periapsis: 82.4396 deg
Mean anomaly: 279.2618 deg
Mean motion: 14.14657025 rev/day
Mean motion (dot): 0.00008001 rev/day2
B* drag term: 0.0038003789 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 5:45 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22474U 92093FP 25346.23987582 .00008001 00000-0 38004-2 0 9992
TLE line 2: 2 22474 71.2997 288.6599 0140108 82.4396 279.2618 14.14657025663880
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
...
Latest news about this satellite
There are no fresh news available about this satellite. Check back as we update our databases every day.
Newsletter sign-up
Weekly statistics, charts and insights to help you stay on top of the space industry.
