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
70.8
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: 1992-093GD
Object number (NORAD): 22494
Object ID (CCSDS): 22494
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.008 minutes
Inclination: 70.8102 deg
SMA: 7231.878 km
Apoapsis: 964.252 km
Periapsis: 743.234 km
RAAN: 116.8991 deg
Eccentricy: 0.01528084
Argument of periapsis: 340.6253 deg
Mean anomaly: 76.6972 deg
Mean motion: 14.11647073 rev/day
Mean motion (dot): 0.00005896 rev/day2
B* drag term: 0.0029255017 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, 10:49 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22494U 92093GD 25347.45111843 .00005896 00000-0 29255-2 0 9995
TLE line 2: 2 22494 70.8102 116.8991 0152808 340.6253 76.6972 14.11647073662985
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.
