Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11123
Days in orbit
Revolutions
≈ 14.6
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: 98.31 minutes
Inclination: 70.9941 deg
SMA: 7055.994 km
Apoapsis: 711.531 km
Periapsis: 644.188 km
RAAN: 285.0493 deg
Eccentricy: 0.0047721
Argument of periapsis: 208.3464 deg
Mean anomaly: 219.1632 deg
Mean motion: 14.64756431 rev/day
Mean motion (dot): 0.00005759 rev/day2
B* drag term: 0.0010723 1/REarth
Two-line elements (TLE)
Creation date: May 7, 2025, 10:46 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 6, 2025, 12:25 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 27760U 94077M 25126.51769528 .00005759 00000-0 10723-2 0 9999
TLE line 2: 2 27760 70.9941 285.0493 0047721 208.3464 219.1632 14.64756431330431
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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