Key statistics
Satellite SL-16 DEB at a glance.
Uptime
9351
Days in orbit
Revolutions
≈ 13.8
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: 2000-006E
Object number (NORAD): 26075
Object ID (CCSDS): 26075
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.628 minutes
Inclination: 71.066 deg
SMA: 7355.183 km
Apoapsis: 1116.236 km
Periapsis: 837.861 km
RAAN: 357.8105 deg
Eccentricy: 0.01892373
Argument of periapsis: 4.6341 deg
Mean anomaly: 17.9835 deg
Mean motion: 13.76298067 rev/day
Mean motion (dot): 0.00000065 rev/day2
B* drag term: 0.000097093068 1/REarth
Two-line elements (TLE)
Creation date: Sept. 9, 2025, 10:35 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 9, 2025, 6:07 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 26075U 00006E 25252.25487551 .00000065 00000-0 97093-4 0 9992
TLE line 2: 2 26075 71.0660 357.8105 0189237 4.6341 17.9835 13.76298067285275
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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