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 43596U 98067PH 20344.36554324 .08904132 12494-4 57179-3 0 9995
2 43596 51.6062 99.6513 0006261 312.7483 99.6145 16.40921535132742
| Epoch (UTC): | 09 December 2020 08:46:22 |
| Eccentricity: | 0.0006261 |
| inclination: | 51.6062° |
| perigee height: | 159 km |
| apogee height: | 167 km |
| right ascension of ascending node: | 99.6513° |
| argument of perigee: | 312.7483° |
| revolutions per day: | 16.40921535 |
| mean anomaly at epoch: | 99.6145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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