Key statistics
Satellite SL-16 DEB at a glance.
Uptime
7697
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: 103.649 minutes
Inclination: 71.0952 deg
SMA: 7309.194 km
Apoapsis: 1059.218 km
Periapsis: 802.9 km
RAAN: 315.0915 deg
Eccentricy: 0.0175339
Argument of periapsis: 86.7489 deg
Mean anomaly: 275.3663 deg
Mean motion: 13.89308023 rev/day
Mean motion (dot): 0.00001249 rev/day2
B* drag term: 0.00093751 1/REarth
Two-line elements (TLE)
Creation date: July 3, 2025, 10:26 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 3, 2025, 3:25 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 32006U 04021J 25184.64287138 .00001249 00000-0 93751-3 0 9991
TLE line 2: 2 32006 71.0952 315.0915 0175339 86.7489 275.3663 13.89308023 50487
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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