Key statistics
Satellite SL-16 DEB at a glance.
Uptime
9340
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: 104.756 minutes
Inclination: 71.0761 deg
SMA: 7361.168 km
Apoapsis: 1125.711 km
Periapsis: 840.355 km
RAAN: 79.7229 deg
Eccentricy: 0.01938247
Argument of periapsis: 11.8303 deg
Mean anomaly: 94.2744 deg
Mean motion: 13.74619998 rev/day
Mean motion (dot): 0.00000016 rev/day2
B* drag term: 0.000053313011 1/REarth
Two-line elements (TLE)
Creation date: Aug. 29, 2025, 2:15 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 28, 2025, 10:21 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 26073U 00006C 25240.93190076 .00000016 00000-0 53313-4 0 9998
TLE line 2: 2 26073 71.0761 79.7229 0193825 11.8303 94.2744 13.74619998282281
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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