Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11953
Days in orbit
Revolutions
≈ 14.1
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: 1993-016BF
Object number (NORAD): 39881
Object ID (CCSDS): 39881
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.25 minutes
Inclination: 70.9898 deg
SMA: 7243.297 km
Apoapsis: 955.946 km
Periapsis: 774.379 km
RAAN: 299.1827 deg
Eccentricy: 0.01253346
Argument of periapsis: 294.2654 deg
Mean anomaly: 64.5413 deg
Mean motion: 14.08310104 rev/day
Mean motion (dot): 0.00003423 rev/day2
B* drag term: 0.0018870591 1/REarth
Two-line elements (TLE)
Creation date: Nov. 22, 2025, 6:56 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Nov. 22, 2025, 6:39 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39881U 93016BF 25326.27768861 .00003423 00000-0 18871-2 0 9990
TLE line 2: 2 39881 70.9898 299.1827 0125335 294.2654 64.5413 14.08310104568386
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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