Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11343
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: 102.94 minutes
Inclination: 70.8819 deg
SMA: 7275.836 km
Apoapsis: 964.448 km
Periapsis: 830.953 km
RAAN: 36.9371 deg
Eccentricy: 0.00917388
Argument of periapsis: 204.2507 deg
Mean anomaly: 155.4276 deg
Mean motion: 13.98873467 rev/day
Mean motion (dot): 0.00000264 rev/day2
B* drag term: 0.00020768373 1/REarth
Two-line elements (TLE)
Creation date: Dec. 14, 2025, 3:07 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 13, 2025, 2:14 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23409U 94077F 25347.59345139 .00000264 00000-0 20768-3 0 9993
TLE line 2: 2 23409 70.8819 36.9371 0091739 204.2507 155.4276 13.98873467584183
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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