Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11792
Days in orbit
Revolutions
≈ 14.1
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.7
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: 1993-016AP
Object number (NORAD): 29100
Object ID (CCSDS): 29100
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.012 minutes
Inclination: 70.7291 deg
SMA: 7232.031 km
Apoapsis: 906.925 km
Periapsis: 800.867 km
RAAN: 92.4117 deg
Eccentricy: 0.0073325
Argument of periapsis: 228.4734 deg
Mean anomaly: 131.008 deg
Mean motion: 14.11602212 rev/day
Mean motion (dot): 0.0000079 rev/day2
B* drag term: 0.00045048 1/REarth
Two-line elements (TLE)
Creation date: July 3, 2025, 5:26 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 3, 2025, 2:32 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 29100U 93016AP 25184.10619419 .00000790 00000-0 45048-3 0 9992
TLE line 2: 2 29100 70.7291 92.4117 0073325 228.4734 131.0080 14.11602212182143
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 13’, on board a Zenit-2 space rocket.
The launch took place on March 26, 1993, 2:21 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 13
Agency: N/A
Status: Launch Successful
Launch date: March 26, 1993, 2:21 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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