Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11290
Days in orbit
Revolutions
≈ 14.0
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.9
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: 1994-077F
Object number (NORAD): 23409
Object ID (CCSDS): 23409
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 102.943 minutes
Inclination: 70.8789 deg
SMA: 7275.979 km
Apoapsis: 965.459 km
Periapsis: 830.229 km
RAAN: 145.5081 deg
Eccentricy: 0.0092929
Argument of periapsis: 279.4929 deg
Mean anomaly: 79.5691 deg
Mean motion: 13.98832272 rev/day
Mean motion (dot): 0.00000269 rev/day2
B* drag term: 0.00021175 1/REarth
Two-line elements (TLE)
Creation date: Oct. 22, 2025, 12:06 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 21, 2025, 7:41 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23409U 94077F 25294.82049160 .00000269 00000-0 21175-3 0 9993
TLE line 2: 2 23409 70.8789 145.5081 0092929 279.4929 79.5691 13.98832272576804
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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