Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11732
Days in orbit
Revolutions
≈ 13.9
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: 1993-016P
Object number (NORAD): 22605
Object ID (CCSDS): 22605
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.527 minutes
Inclination: 70.9967 deg
SMA: 7303.458 km
Apoapsis: 1021.556 km
Periapsis: 829.09 km
RAAN: 76.964 deg
Eccentricy: 0.0131764
Argument of periapsis: 269.6435 deg
Mean anomaly: 157.0477 deg
Mean motion: 13.90945011 rev/day
Mean motion (dot): 0.0000028 rev/day2
B* drag term: 0.00024221 1/REarth
Two-line elements (TLE)
Creation date: May 9, 2025, 2:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 7, 2025, 11:35 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22605U 93016P 25127.98315307 .00000280 00000-0 24221-3 0 9991
TLE line 2: 2 22605 70.9967 76.9640 0131764 269.6435 157.0477 13.90945011627935
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
In-orbit conjunctions
A list of the most updated potential collisions computed for object 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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