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 43551U 98067NZ 20289.40008140 .12819970 12606-4 34454-3 0 9995
2 43551 51.6143 6.3935 0004068 320.9805 39.0930 16.45548142129489
| Epoch (UTC): | 15 October 2020 09:36:07 |
| Eccentricity: | 0.0004068 |
| inclination: | 51.6143° |
| perigee height: | 148 km |
| apogee height: | 154 km |
| right ascension of ascending node: | 6.3935° |
| argument of perigee: | 320.9805° |
| revolutions per day: | 16.45548142 |
| mean anomaly at epoch: | 39.0930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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