Key statistics
Satellite SL-16 DEB at a glance.
Uptime
9285
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.1
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: 2000-006C
Object number (NORAD): 26073
Object ID (CCSDS): 26073
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.757 minutes
Inclination: 71.0755 deg
SMA: 7361.209 km
Apoapsis: 1124.315 km
Periapsis: 841.832 km
RAAN: 186.3428 deg
Eccentricy: 0.0191873
Argument of periapsis: 90.5293 deg
Mean anomaly: 57.839 deg
Mean motion: 13.74608677 rev/day
Mean motion (dot): 0.00000093 rev/day2
B* drag term: 0.00012384 1/REarth
Two-line elements (TLE)
Creation date: July 5, 2025, 5:45 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 5, 2025, 10:28 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 26073U 00006C 25186.43666734 .00000093 00000-0 12384-3 0 9998
TLE line 2: 2 26073 71.0755 186.3428 0191873 90.5293 57.8390 13.74608677274794
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 21’, on board a Zenit-2 space rocket.
The launch took place on Feb. 3, 2000, 9:26 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 21
Agency: N/A
Status: Launch Successful
Launch date: Feb. 3, 2000, 9:26 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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