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 43340U 18036B 20173.78783517 0.00000000 00000-0 00000-0 0 04
2 43340 1.0720 93.3151 0002630 18.6158 341.3842 0.99183136 03
| Epoch (UTC): | 21 June 2020 18:54:28 |
| Eccentricity: | 0.0002630 |
| inclination: | 1.0720° |
| perigee height: | 36083 km |
| apogee height: | 36105 km |
| right ascension of ascending node: | 93.3151° |
| argument of perigee: | 18.6158° |
| revolutions per day: | 0.99183136 |
| mean anomaly at epoch: | 341.3842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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