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 42072U 17015A 22259.89490036 0.00000000 00000-0 00000-0 0 01
2 42072 97.3685 329.6664 0001676 351.6423 8.3427 15.25981446 04
| Epoch (UTC): | 16 September 2022 21:28:39 |
| Eccentricity: | 0.0001676 |
| inclination: | 97.3685° |
| perigee height: | 486 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 329.6664° |
| argument of perigee: | 351.6423° |
| revolutions per day: | 15.25981446 |
| mean anomaly at epoch: | 8.3427° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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