Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11821
Days in orbit
Revolutions
≈ 14.1
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: 1992-093DH
Object number (NORAD): 22416
Object ID (CCSDS): 22416
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 102.409 minutes
Inclination: 70.9593 deg
SMA: 7250.778 km
Apoapsis: 931.355 km
Periapsis: 813.932 km
RAAN: 267.2145 deg
Eccentricy: 0.0080973
Argument of periapsis: 239.0983 deg
Mean anomaly: 243.7503 deg
Mean motion: 14.06131102 rev/day
Mean motion (dot): 0.00000086 rev/day2
B* drag term: 0.000078814 1/REarth
Two-line elements (TLE)
Creation date: May 7, 2025, 3:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 6, 2025, 7:59 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22416U 92093DH 25126.83305650 .00000086 00000-0 78814-4 0 9990
TLE line 2: 2 22416 70.9593 267.2145 0080973 239.0983 243.7503 14.06131102658505
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
In-orbit conjunctions
A list of the most updated potential collisions computed for object 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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