Key statistics
Satellite SL-16 DEB at a glance.
Uptime
9387
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: 104.755 minutes
Inclination: 71.0797 deg
SMA: 7361.114 km
Apoapsis: 1127.227 km
Periapsis: 838.731 km
RAAN: 345.8627 deg
Eccentricy: 0.01959592
Argument of periapsis: 303.2433 deg
Mean anomaly: 237.7186 deg
Mean motion: 13.74635105 rev/day
Mean motion (dot): 0.00000185 rev/day2
B* drag term: 0.00020927548 1/REarth
Two-line elements (TLE)
Creation date: Oct. 16, 2025, 2:37 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 15, 2025, 9:37 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 26073U 00006C 25288.90123067 .00000185 00000-0 20928-3 0 9995
TLE line 2: 2 26073 71.0797 345.8627 0195959 303.2433 237.7186 13.74635105288874
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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