Key statistics
Satellite SL-16 DEB at a glance.
Uptime
9404
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
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: 2000-006G
Object number (NORAD): 26077
Object ID (CCSDS): 26077
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.86 minutes
Inclination: 70.968 deg
SMA: 7366.014 km
Apoapsis: 1136.567 km
Periapsis: 839.19 km
RAAN: 255.5322 deg
Eccentricy: 0.02018577
Argument of periapsis: 109.7366 deg
Mean anomaly: 66.5066 deg
Mean motion: 13.73263856 rev/day
Mean motion (dot): 0.00000089 rev/day2
B* drag term: 0.00012148001 1/REarth
Two-line elements (TLE)
Creation date: Nov. 1, 2025, 7:40 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Nov. 1, 2025, 3:34 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 26077U 00006G 25305.64913469 .00000089 00000-0 12148-3 0 9991
TLE line 2: 2 26077 70.9680 255.5322 0201858 109.7366 66.5066 13.73263856289758
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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