Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11287
Days in orbit
Revolutions
≈ 13.7
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: 1994-077E
Object number (NORAD): 23408
Object ID (CCSDS): 23408
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 105.012 minutes
Inclination: 70.9855 deg
SMA: 7373.147 km
Apoapsis: 1151.957 km
Periapsis: 838.066 km
RAAN: 189.3114 deg
Eccentricy: 0.02128612
Argument of periapsis: 11.4194 deg
Mean anomaly: 0.1501 deg
Mean motion: 13.71271479 rev/day
Mean motion (dot): 0.00000203 rev/day2
B* drag term: 0.00023281105 1/REarth
Two-line elements (TLE)
Creation date: Oct. 19, 2025, 2:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 18, 2025, 11:40 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23408U 94077E 25291.98634222 .00000203 00000-0 23281-3 0 9993
TLE line 2: 2 23408 70.9855 189.3114 0212861 11.4194 0.1501 13.71271479545654
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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