Key statistics
Satellite SL-16 DEB at a glance.
Uptime
7639
Days in orbit
Revolutions
≈ 13.9
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: 2004-021J
Object number (NORAD): 32006
Object ID (CCSDS): 32006
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.665 minutes
Inclination: 71.0955 deg
SMA: 7309.963 km
Apoapsis: 1060.028 km
Periapsis: 803.628 km
RAAN: 67.462 deg
Eccentricy: 0.0175377
Argument of periapsis: 169.9719 deg
Mean anomaly: 190.4968 deg
Mean motion: 13.8908864 rev/day
Mean motion (dot): 0.00002042 rev/day2
B* drag term: 0.0015187 1/REarth
Two-line elements (TLE)
Creation date: May 9, 2025, 2:46 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 8, 2025, 1:13 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 32006U 04021J 25128.55079361 .00002042 00000-0 15187-2 0 9994
TLE line 2: 2 32006 71.0955 67.4620 0175377 169.9719 190.4968 13.89088640600276
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
In-orbit conjunctions
A list of the most updated potential collisions computed for object SL-16 DEB.
Associated space launch
Second generation ELING satellite
SL-16 DEB was lifted into orbit during the mission ‘Zenit-2 | Tselina-2 22’, on board a Zenit-2 space rocket.
The launch took place on June 10, 2004, 1:28 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 22
Agency: N/A
Status: Launch Successful
Launch date: June 10, 2004, 1:28 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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