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 4579U 70083B 22228.01816446 .00000186 00000-0 44314-4 0 9994
2 4579 74.0013 83.2626 0010504 347.7115 12.3793 14.60721016750080
| Epoch (UTC): | 16 August 2022 00:26:09 |
| Eccentricity: | 0.0010504 |
| inclination: | 74.0013° |
| perigee height: | 683 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 83.2626° |
| argument of perigee: | 347.7115° |
| revolutions per day: | 14.60721016 |
| mean anomaly at epoch: | 12.3793° |
| orbit number at epoch: | 75008 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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