Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11127
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: 105.015 minutes
Inclination: 70.9831 deg
SMA: 7373.298 km
Apoapsis: 1153.738 km
Periapsis: 836.588 km
RAAN: 143.1233 deg
Eccentricy: 0.0215067
Argument of periapsis: 238.8883 deg
Mean anomaly: 275.9736 deg
Mean motion: 13.7122928 rev/day
Mean motion (dot): 0.0000009 rev/day2
B* drag term: 0.00012644 1/REarth
Two-line elements (TLE)
Creation date: May 11, 2025, 10:21 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 11, 2025, 11 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23408U 94077E 25131.45847928 .00000090 00000-0 12644-3 0 9992
TLE line 2: 2 23408 70.9831 143.1233 0215067 238.8883 275.9736 13.71229280523649
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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