Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11882
Days in orbit
Revolutions
≈ 14.1
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: 1992-093JP
Object number (NORAD): 28042
Object ID (CCSDS): 28042
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.887 minutes
Inclination: 70.8738 deg
SMA: 7226.112 km
Apoapsis: 900.456 km
Periapsis: 795.498 km
RAAN: 356.4479 deg
Eccentricy: 0.0072624
Argument of periapsis: 266.5983 deg
Mean anomaly: 124.2524 deg
Mean motion: 14.1333702 rev/day
Mean motion (dot): 0.00000315 rev/day2
B* drag term: 0.00018925 1/REarth
Two-line elements (TLE)
Creation date: July 6, 2025, 6:05 p.m.
Reference frame: TEME
Reference center: EARTH
Epoch: July 6, 2025, 11:26 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 28042U 92093JP 25187.47689380 .00000315 00000-0 18925-3 0 9994
TLE line 2: 2 28042 70.8738 356.4479 0072624 266.5983 124.2524 14.13337020463994
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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