Key statistics
Satellite SL-16 DEB at a glance.
Uptime
6743
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.9
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: 2007-029S
Object number (NORAD): 43375
Object ID (CCSDS): 43375
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.67 minutes
Inclination: 70.8883 deg
SMA: 7215.849 km
Apoapsis: 918.322 km
Periapsis: 757.105 km
RAAN: 309.3512 deg
Eccentricy: 0.011171
Argument of periapsis: 254.8879 deg
Mean anomaly: 284.514 deg
Mean motion: 14.1635342 rev/day
Mean motion (dot): 0.00007609 rev/day2
B* drag term: 0.0036243 1/REarth
Two-line elements (TLE)
Creation date: Dec. 9, 2025, 11:46 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 9, 2025, 3:37 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 43375U 07029S 25343.65091123 .00007609 00000-0 36243-2 0 9996
TLE line 2: 2 43375 70.8883 309.3512 0111710 254.8879 284.5140 14.16353420617259
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 2M | Tselina-2 23’, on board a Zenit 2M space rocket.
The launch took place on June 29, 2007, 10 a.m. from 45/1.
For more information about the launch, click the button.
Zenit 2M | Tselina-2 23
Agency: N/A
Status: Launch Successful
Launch date: June 29, 2007, 10 a.m. UTC
Rocket: Zenit 2M
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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