Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11183
Days in orbit
Revolutions
≈ 14.7
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: 1994-077M
Object number (NORAD): 27760
Object ID (CCSDS): 27760
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 98.28 minutes
Inclination: 70.9934 deg
SMA: 7054.581 km
Apoapsis: 707.534 km
Periapsis: 645.358 km
RAAN: 145.9732 deg
Eccentricy: 0.0044068
Argument of periapsis: 107.5227 deg
Mean anomaly: 8.2352 deg
Mean motion: 14.65196659 rev/day
Mean motion (dot): 0.00003255 rev/day2
B* drag term: 0.00060667 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, 1:40 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 27760U 94077M 25187.56959756 .00003255 00000-0 60667-3 0 9997
TLE line 2: 2 27760 70.9934 145.9732 0044068 107.5227 8.2352 14.65196659339369
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 16’, on board a Zenit-2 space rocket.
The launch took place on Nov. 24, 1994, 9:15 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 16
Agency: N/A
Status: Launch Successful
Launch date: Nov. 24, 1994, 9:15 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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