Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11852
Days in orbit
Revolutions
≈ 13.8
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: 1993-016N
Object number (NORAD): 22604
Object ID (CCSDS): 22604
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 104.615 minutes
Inclination: 70.995 deg
SMA: 7354.544 km
Apoapsis: 1099.81 km
Periapsis: 853.008 km
RAAN: 324.6529 deg
Eccentricy: 0.0167789
Argument of periapsis: 123.5357 deg
Mean anomaly: 56.3176 deg
Mean motion: 13.76477525 rev/day
Mean motion (dot): 0.00000015 rev/day2
B* drag term: 0.000052462202 1/REarth
Two-line elements (TLE)
Creation date: Sept. 6, 2025, 2:09 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 5, 2025, 11:15 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22604U 93016N 25248.96895324 .00000015 00000-0 52462-4 0 9999
TLE line 2: 2 22604 70.9950 324.6529 0167789 123.5357 56.3176 13.76477525629913
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 13’, on board a Zenit-2 space rocket.
The launch took place on March 26, 1993, 2:21 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 13
Agency: N/A
Status: Launch Successful
Launch date: March 26, 1993, 2:21 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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