Key statistics
Satellite SL-16 DEB at a glance.
Uptime
9842
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: 1998-045D
Object number (NORAD): 25410
Object ID (CCSDS): 25410
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.998 minutes
Inclination: 70.9809 deg
SMA: 7372.485 km
Apoapsis: 1148.878 km
Periapsis: 839.823 km
RAAN: 355.9524 deg
Eccentricy: 0.02096
Argument of periapsis: 268.8425 deg
Mean anomaly: 167.2764 deg
Mean motion: 13.71456044 rev/day
Mean motion (dot): 0.00000031 rev/day2
B* drag term: 0.00007173 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 3:21 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 25410U 98045D 25187.63981205 .00000031 00000-0 71730-4 0 9991
TLE line 2: 2 25410 70.9809 355.9524 0209600 268.8425 167.2764 13.71456044347611
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 20’, on board a Zenit-2 space rocket.
The launch took place on July 28, 1998, 9:15 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 20
Agency: N/A
Status: Launch Successful
Launch date: July 28, 1998, 9:15 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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