Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11730
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: 1993-016S
Object number (NORAD): 22608
Object ID (CCSDS): 22608
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 103.994 minutes
Inclination: 71.004 deg
SMA: 7325.414 km
Apoapsis: 1041.588 km
Periapsis: 852.969 km
RAAN: 258.8022 deg
Eccentricy: 0.0128743
Argument of periapsis: 62.1533 deg
Mean anomaly: 92.6941 deg
Mean motion: 13.84696335 rev/day
Mean motion (dot): 0.00000015 rev/day2
B* drag term: 0.000048863 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, 7:09 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22608U 93016S 25125.79797479 .00000015 00000-0 48863-4 0 9990
TLE line 2: 2 22608 71.0040 258.8022 0128743 62.1533 92.6941 13.84696335622542
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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