Key statistics
Satellite SL-16 DEB at a glance.
Uptime
11854
Days in orbit
Revolutions
≈ 14.4
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: 1993-016E
Object number (NORAD): 22577
Object ID (CCSDS): 22577
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: MEDIUM
Orbital parameters
Period: 99.739 minutes
Inclination: 71.0385 deg
SMA: 7124.211 km
Apoapsis: 828.391 km
Periapsis: 663.76 km
RAAN: 225.4154 deg
Eccentricy: 0.01155427
Argument of periapsis: 168.4562 deg
Mean anomaly: 4.3008 deg
Mean motion: 14.43768783 rev/day
Mean motion (dot): 0.00000141 rev/day2
B* drag term: 0.000053344868 1/REarth
Two-line elements (TLE)
Creation date: Sept. 8, 2025, 3:16 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 7, 2025, 4:08 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 22577U 93016E 25250.67249472 .00000141 00000-0 53345-4 0 9997
TLE line 2: 2 22577 71.0385 225.4154 0115543 168.4562 4.3008 14.43768783708262
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 13’, on board a Zenit-2 space rocket.
The launch took place on March 26, 1993, 2:21 a.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 13
Agency: N/A
Status: Launch Successful
Launch date: March 26, 1993, 2:21 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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