Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11729
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: 102.327 minutes
Inclination: 70.9888 deg
SMA: 7246.908 km
Apoapsis: 957.223 km
Periapsis: 780.323 km
RAAN: 4.8039 deg
Eccentricy: 0.0122052
Argument of periapsis: 241.9489 deg
Mean anomaly: 116.9244 deg
Mean motion: 14.07257679 rev/day
Mean motion (dot): 0.00002743 rev/day2
B* drag term: 0.0015532 1/REarth
Two-line elements (TLE)
Creation date: May 2, 2025, 2:33 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 1, 2025, 8:18 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 39881U 93016BF 25121.34620660 .00002743 00000-0 15532-2 0 9990
TLE line 2: 2 39881 70.9888 4.8039 0122052 241.9489 116.9244 14.07257679539545
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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