Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11951
Days in orbit
Revolutions
≈ 14.0
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: 1993-016BV
Object number (NORAD): 39895
Object ID (CCSDS): 39895
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.146 minutes
Inclination: 70.9883 deg
SMA: 7285.538 km
Apoapsis: 997.617 km
Periapsis: 817.188 km
RAAN: 217.9188 deg
Eccentricy: 0.01238267
Argument of periapsis: 230.4959 deg
Mean anomaly: 128.5155 deg
Mean motion: 13.96080096 rev/day
Mean motion (dot): 0.00000506 rev/day2
B* drag term: 0.00037725753 1/REarth
Two-line elements (TLE)
Creation date: Dec. 13, 2025, 4:32 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 10:15 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39895U 93016BV 25346.92712794 .00000506 00000-0 37726-3 0 9993
TLE line 2: 2 39895 70.9883 217.9188 0123827 230.4959 128.5155 13.96080096307922
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-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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