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 40208U 14055A 20180.20928624 0.00000000 00000-0 00000-0 0 06
2 40208 0.0961 120.8977 0014997 230.4577 129.3781 1.00281279 05
| Epoch (UTC): | 28 June 2020 05:01:22 |
| Eccentricity: | 0.0014997 |
| inclination: | 0.0961° |
| perigee height: | 35720 km |
| apogee height: | 35847 km |
| right ascension of ascending node: | 120.8977° |
| argument of perigee: | 230.4577° |
| revolutions per day: | 1.00281279 |
| mean anomaly at epoch: | 129.3781° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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