Key statistics
Satellite SL-16 DEB at a glance.
Uptime
6641
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: 2007-029C
Object number (NORAD): 31794
Object ID (CCSDS): 31794
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.98 minutes
Inclination: 71.0432 deg
SMA: 7371.632 km
Apoapsis: 1145.098 km
Periapsis: 841.895 km
RAAN: 138.0616 deg
Eccentricy: 0.02056556
Argument of periapsis: 356.4278 deg
Mean anomaly: 69.4341 deg
Mean motion: 13.71694299 rev/day
Mean motion (dot): 0.00000338 rev/day2
B* drag term: 0.00036267567 1/REarth
Two-line elements (TLE)
Creation date: Sept. 3, 2025, 2:21 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 2, 2025, 5:29 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 31794U 07029C 25245.72906403 .00000338 00000-0 36268-3 0 9993
TLE line 2: 2 31794 71.0432 138.0616 0205656 356.4278 69.4341 13.71694299909924
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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