Key statistics
Satellite SL-16 DEB at a glance.
Uptime
6526
Days in orbit
Revolutions
≈ 13.7
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: 2007-029F
Object number (NORAD): 31799
Object ID (CCSDS): 31799
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 105.39 minutes
Inclination: 70.945 deg
SMA: 7390.844 km
Apoapsis: 1179.594 km
Periapsis: 845.825 km
RAAN: 49.7817 deg
Eccentricy: 0.0225799
Argument of periapsis: 6.7222 deg
Mean anomaly: 142.4395 deg
Mean motion: 13.66349193 rev/day
Mean motion (dot): 0.00000086 rev/day2
B* drag term: 0.00012993 1/REarth
Two-line elements (TLE)
Creation date: May 10, 2025, 5:27 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 10, 2025, 5:02 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 31799U 07029F 25130.21005119 .00000086 00000-0 12993-3 0 9998
TLE line 2: 2 31799 70.9450 49.7817 0225799 6.7222 142.4395 13.66349193890342
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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