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 data is extracted from the following two-line orbital elements,
1 44768C 19074BH 21021.40783988 .00008060 00000-0 54004-3 0 219
2 44768 53.0571 356.0902 0002090 55.8850 66.5255 15.06391152 12
| Epoch (UTC): | 21 January 2021 09:47:17 |
| Eccentricity: | 0.0002090 |
| inclination: | 53.0571° |
| perigee height: | 546 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 356.0902° |
| argument of perigee: | 55.8850° |
| revolutions per day: | 15.06391152 |
| mean anomaly at epoch: | 66.5255° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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