Key statistics
Satellite SL-16 DEB at a glance.
Uptime
9287
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: 104.63 minutes
Inclination: 71.0628 deg
SMA: 7355.243 km
Apoapsis: 1114.749 km
Periapsis: 839.466 km
RAAN: 122.2396 deg
Eccentricy: 0.0187134
Argument of periapsis: 96.293 deg
Mean anomaly: 322.6306 deg
Mean motion: 13.7628146 rev/day
Mean motion (dot): 0.00000101 rev/day2
B* drag term: 0.00012808 1/REarth
Two-line elements (TLE)
Creation date: July 8, 2025, 2:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 7, 2025, 9:14 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 26075U 00006E 25188.88513247 .00000101 00000-0 12808-3 0 9992
TLE line 2: 2 26075 71.0628 122.2396 0187134 96.2930 322.6306 13.76281460276559
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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