View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 43465U 18036G 19350.26980955 0.00000000 00000-0 00000-0 0 05
2 43465 0.5829 96.2443 0000515 331.1216 20.0587 0.99175680 01
| Epoch (UTC): | 16 December 2019 06:28:31 |
| Eccentricity: | 0.0000515 |
| inclination: | 0.5829° |
| perigee height: | 36094 km |
| apogee height: | 36098 km |
| right ascension of ascending node: | 96.2443° |
| argument of perigee: | 331.1216° |
| revolutions per day: | 0.99175680 |
| mean anomaly at epoch: | 20.0587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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