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 43021U 98067NJ 21161.58356675 .11371101 12760-4 85574-4 0 9994
2 43021 51.6049 216.0033 0005565 279.2361 80.8041 16.52395905203598
| Epoch (UTC): | 10 June 2021 14:00:20 |
| Eccentricity: | 0.0005565 |
| inclination: | 51.6049° |
| perigee height: | 129 km |
| apogee height: | 136 km |
| right ascension of ascending node: | 216.0033° |
| argument of perigee: | 279.2361° |
| revolutions per day: | 16.52395905 |
| mean anomaly at epoch: | 80.8041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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