Key statistics
Satellite SL-16 DEB at a glance.
Uptime
9779
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: 104.999 minutes
Inclination: 70.9773 deg
SMA: 7372.523 km
Apoapsis: 1147.831 km
Periapsis: 840.945 km
RAAN: 117.0392 deg
Eccentricy: 0.0208128
Argument of periapsis: 355.5711 deg
Mean anomaly: 188.3899 deg
Mean motion: 13.71445523 rev/day
Mean motion (dot): 0.00000212 rev/day2
B* drag term: 0.00024278 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 5:43 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 25410U 98045D 25125.73879372 .00000212 00000-0 24278-3 0 9990
TLE line 2: 2 25410 70.9773 117.0392 0208128 355.5711 188.3899 13.71445523339127
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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