Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11820
Days in orbit
Revolutions
≈ 14.0
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: 1992-093EX
Object number (NORAD): 22458
Object ID (CCSDS): 22458
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.676 minutes
Inclination: 70.8526 deg
SMA: 7263.375 km
Apoapsis: 936.924 km
Periapsis: 833.556 km
RAAN: 305.8979 deg
Eccentricy: 0.0071157
Argument of periapsis: 119.8358 deg
Mean anomaly: 60.0828 deg
Mean motion: 14.02474669 rev/day
Mean motion (dot): 0.00000342 rev/day2
B* drag term: 0.0002474 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 6:21 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22458U 92093EX 25125.26523238 .00000342 00000-0 24740-3 0 9999
TLE line 2: 2 22458 70.8526 305.8979 0071157 119.8358 60.0828 14.02474669651603
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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