Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11243
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: 102.945 minutes
Inclination: 70.8784 deg
SMA: 7276.093 km
Apoapsis: 964.561 km
Periapsis: 831.356 km
RAAN: 243.3309 deg
Eccentricy: 0.00915359
Argument of periapsis: 347.555 deg
Mean anomaly: 12.3302 deg
Mean motion: 13.98799152 rev/day
Mean motion (dot): 0.00000377 rev/day2
B* drag term: 0.00028382132 1/REarth
Two-line elements (TLE)
Creation date: Sept. 4, 2025, 10:13 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 4, 2025, 6:23 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23409U 94077F 25247.26665480 .00000377 00000-0 28382-3 0 9995
TLE line 2: 2 23409 70.8784 243.3309 0091536 347.5550 12.3302 13.98799152570154
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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