Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11246
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: 98.246 minutes
Inclination: 70.997 deg
SMA: 7052.952 km
Apoapsis: 707.433 km
Periapsis: 642.202 km
RAAN: 4.2113 deg
Eccentricy: 0.0046244
Argument of periapsis: 1.2555 deg
Mean anomaly: 124.1495 deg
Mean motion: 14.65704177 rev/day
Mean motion (dot): 0.00005864 rev/day2
B* drag term: 0.0010697917 1/REarth
Two-line elements (TLE)
Creation date: Sept. 7, 2025, 3:09 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 6, 2025, 6:10 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 27760U 94077M 25249.75706882 .00005864 00000-0 10698-2 0 9993
TLE line 2: 2 27760 70.9970 4.2113 0046244 1.2555 124.1495 14.65704177348479
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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