Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11881
Days in orbit
Revolutions
≈ 14.4
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.2
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: 1992-093JM
Object number (NORAD): 27750
Object ID (CCSDS): 27750
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 100.272 minutes
Inclination: 71.1539 deg
SMA: 7149.562 km
Apoapsis: 828.322 km
Periapsis: 714.531 km
RAAN: 117.9779 deg
Eccentricy: 0.0079579
Argument of periapsis: 96.2042 deg
Mean anomaly: 264.8166 deg
Mean motion: 14.36096529 rev/day
Mean motion (dot): 0.00003536 rev/day2
B* drag term: 0.0011863 1/REarth
Two-line elements (TLE)
Creation date: July 3, 2025, 10:26 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 3, 2025, 12:58 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 27750U 92093JM 25184.54063120 .00003536 00000-0 11863-2 0 9993
TLE line 2: 2 27750 71.1539 117.9779 0079579 96.2042 264.8166 14.36096529227740
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 12’, on board a Zenit-2 space rocket.
The launch took place on Dec. 25, 1992, 5:56 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 12
Agency: N/A
Status: Launch Successful
Launch date: Dec. 25, 1992, 5:56 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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