Key statistics
Satellite SL-16 DEB at a glance.
Uptime
12769
Days in orbit
Revolutions
≈ 13.7
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: 1990-046D
Object number (NORAD): 20627
Object ID (CCSDS): 20627
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 105.042 minutes
Inclination: 70.9732 deg
SMA: 7374.552 km
Apoapsis: 1152.663 km
Periapsis: 840.171 km
RAAN: 305.5715 deg
Eccentricy: 0.0211872
Argument of periapsis: 144.8037 deg
Mean anomaly: 329.3395 deg
Mean motion: 13.70879513 rev/day
Mean motion (dot): 0.00000224 rev/day2
B* drag term: 0.00025474 1/REarth
Two-line elements (TLE)
Creation date: May 6, 2025, 3:54 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: May 5, 2025, 8:14 p.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 20627U 90046D 25125.84309116 .00000224 00000-0 25474-3 0 9996
TLE line 2: 2 20627 70.9732 305.5715 0211872 144.8037 329.3395 13.70879513747838
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 7’, on board a Zenit-2 space rocket.
The launch took place on May 22, 1990, 5:14 a.m. from 45/2.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 7
Agency: N/A
Status: Launch Successful
Launch date: May 22, 1990, 5:14 a.m. UTC
Rocket: Zenit-2
Launch pad: 45/2
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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