Key statistics
Satellite SL-16 DEB at a glance.
Uptime
9288
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: 2000-006G
Object number (NORAD): 26077
Object ID (CCSDS): 26077
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.862 minutes
Inclination: 70.9688 deg
SMA: 7366.105 km
Apoapsis: 1139.831 km
Periapsis: 836.108 km
RAAN: 122.7993 deg
Eccentricy: 0.0206163
Argument of periapsis: 272.9947 deg
Mean anomaly: 143.7242 deg
Mean motion: 13.73238425 rev/day
Mean motion (dot): 0.00000003 rev/day2
B* drag term: 0.000043881 1/REarth
Two-line elements (TLE)
Creation date: July 9, 2025, 2:22 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 8, 2025, 9:08 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 26077U 00006G 25189.88100553 .00000003 00000-0 43881-4 0 9994
TLE line 2: 2 26077 70.9688 122.7993 0206163 272.9947 143.7242 13.73238425273860
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 21’, on board a Zenit-2 space rocket.
The launch took place on Feb. 3, 2000, 9:26 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 21
Agency: N/A
Status: Launch Successful
Launch date: Feb. 3, 2000, 9:26 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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