Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11936
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: 101.882 minutes
Inclination: 70.8696 deg
SMA: 7225.876 km
Apoapsis: 898.982 km
Periapsis: 796.499 km
RAAN: 242.6992 deg
Eccentricy: 0.0070914
Argument of periapsis: 187.1641 deg
Mean anomaly: 322.29 deg
Mean motion: 14.13406274 rev/day
Mean motion (dot): 0.00001114 rev/day2
B* drag term: 0.00060384544 1/REarth
Two-line elements (TLE)
Creation date: Aug. 30, 2025, 3:38 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 29, 2025, 10:19 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 28042U 92093JP 25241.42986919 .00001114 00000-0 60385-3 0 9993
TLE line 2: 2 28042 70.8696 242.6992 0070914 187.1641 322.2900 14.13406274471616
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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