Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11001
Days in orbit
Revolutions
≈ 14.2
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: 1995-058G
Object number (NORAD): 24284
Object ID (CCSDS): 24284
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 101.378 minutes
Inclination: 70.8632 deg
SMA: 7202.065 km
Apoapsis: 831.314 km
Periapsis: 816.546 km
RAAN: 79.9496 deg
Eccentricy: 0.00102521
Argument of periapsis: 45.9097 deg
Mean anomaly: 314.2869 deg
Mean motion: 14.20421412 rev/day
Mean motion (dot): 0.00000645 rev/day2
B* drag term: 0.00032354116 1/REarth
Two-line elements (TLE)
Creation date: Dec. 12, 2025, 10:14 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Dec. 12, 2025, 7:17 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 24284U 95058G 25346.30388388 .00000645 00000-0 32354-3 0 9993
TLE line 2: 2 24284 70.8632 79.9496 0010252 45.9097 314.2869 14.20421412557209
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 17’, on board a Zenit-2 space rocket.
The launch took place on Oct. 31, 1995, 8:19 p.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 17
Agency: N/A
Status: Launch Successful
Launch date: Oct. 31, 1995, 8:19 p.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
...
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