Key statistics
Satellite SL-16 DEB * at a glance.
Uptime
11791
Days in orbit
Revolutions
≈ 14.2
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: 1993-016DK
Object number (NORAD): 42255
Object ID (CCSDS): 42255
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.238 minutes
Inclination: 71.0081 deg
SMA: 7195.419 km
Apoapsis: 825.001 km
Periapsis: 809.568 km
RAAN: 311.5223 deg
Eccentricy: 0.0010724
Argument of periapsis: 289.9662 deg
Mean anomaly: 184.9256 deg
Mean motion: 14.2238975 rev/day
Mean motion (dot): 0.00000454 rev/day2
B* drag term: 0.00022546 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 12:48 a.m. UTC
TLE line 0: 0 SL-16 DEB *
TLE line 1: 1 42255U 93016DK 25187.03386782 .00000454 00000-0 22546-3 0 9992
TLE line 2: 2 42255 71.0081 311.5223 0010724 289.9662 184.9256 14.22389750601801
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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