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 04579U 70083B 22229.04547505 .00000185 00000-0 44227-4 0 9997
2 04579 74.0012 81.2959 0010560 345.5695 14.5167 14.60721511750165
| Epoch (UTC): | 17 August 2022 01:05:29 |
| Eccentricity: | 0.0010560 |
| inclination: | 74.0012° |
| perigee height: | 683 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 81.2959° |
| argument of perigee: | 345.5695° |
| revolutions per day: | 14.60721511 |
| mean anomaly at epoch: | 14.5167° |
| orbit number at epoch: | 75016 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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