Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12042
Days in orbit
Revolutions
≈ 13.9
Per day
Orbit
LEO
Low Earth Orbit
Inclination
70.9
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: 1992-093BX
Object number (NORAD): 22382
Object ID (CCSDS): 22382
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 103.478 minutes
Inclination: 70.8656 deg
SMA: 7301.18 km
Apoapsis: 1038.747 km
Periapsis: 807.342 km
RAAN: 152.8423 deg
Eccentricy: 0.0158471
Argument of periapsis: 178.3431 deg
Mean anomaly: 309.9654 deg
Mean motion: 13.91596134 rev/day
Mean motion (dot): 0.00001473 rev/day2
B* drag term: 0.0010811 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 7:26 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 11, 2025, 8:45 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22382U 92093BX 25345.86478802 .00001473 00000-0 10811-2 0 9990
TLE line 2: 2 22382 70.8656 152.8423 0158471 178.3431 309.9654 13.91596134663440
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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