Key statistics
Satellite SL-16 DEB at a glance.
Uptime
9224
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: 104.758 minutes
Inclination: 71.0769 deg
SMA: 7361.262 km
Apoapsis: 1125.983 km
Periapsis: 840.271 km
RAAN: 304.8282 deg
Eccentricy: 0.0194065
Argument of periapsis: 177.8701 deg
Mean anomaly: 253.2019 deg
Mean motion: 13.74593733 rev/day
Mean motion (dot): 0.00000154 rev/day2
B* drag term: 0.00018078 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 9:02 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 26073U 00006C 25125.87686522 .00000154 00000-0 18078-3 0 9990
TLE line 2: 2 26073 71.0769 304.8282 0194065 177.8701 253.2019 13.74593733266475
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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