Key statistics
Satellite SL-16 DEB at a glance.
Uptime
6643
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: 2007-029E
Object number (NORAD): 31796
Object ID (CCSDS): 31796
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 105.199 minutes
Inclination: 71.0433 deg
SMA: 7381.892 km
Apoapsis: 1160.977 km
Periapsis: 846.538 km
RAAN: 197.8737 deg
Eccentricy: 0.02129797
Argument of periapsis: 59.7046 deg
Mean anomaly: 14.5298 deg
Mean motion: 13.68835275 rev/day
Mean motion (dot): 0.00000316 rev/day2
B* drag term: 0.00035304319 1/REarth
Two-line elements (TLE)
Creation date: Sept. 4, 2025, 10:13 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 4, 2025, 12:33 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 31796U 07029E 25247.02315353 .00000316 00000-0 35304-3 0 9994
TLE line 2: 2 31796 71.0433 197.8737 0212980 59.7046 14.5298 13.68835275908274
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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