Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11731
Days in orbit
Revolutions
≈ 13.8
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
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: 1993-016N
Object number (NORAD): 22604
Object ID (CCSDS): 22604
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 104.616 minutes
Inclination: 70.993 deg
SMA: 7354.575 km
Apoapsis: 1102.618 km
Periapsis: 850.262 km
RAAN: 203.13 deg
Eccentricy: 0.0171564
Argument of periapsis: 295.1934 deg
Mean anomaly: 239.3659 deg
Mean motion: 13.76468824 rev/day
Mean motion (dot): -0.00000015 rev/day2
B* drag term: 0.000027169 1/REarth
Two-line elements (TLE)
Creation date: May 8, 2025, 3:01 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 11:19 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22604U 93016N 25127.97179166 -.00000015 00000-0 27169-4 0 9992
TLE line 2: 2 22604 70.9930 203.1300 0171564 295.1934 239.3659 13.76468824613264
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 13’, on board a Zenit-2 space rocket.
The launch took place on March 26, 1993, 2:21 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 13
Agency: N/A
Status: Launch Successful
Launch date: March 26, 1993, 2:21 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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