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 42376U 00055RU 22184.16320533 .00001643 00000-0 12847-2 0 9990
2 42376 98.8550 155.7497 0115690 220.1768 139.0796 13.90434698325715
| Epoch (UTC): | 03 July 2022 03:55:00 |
| Eccentricity: | 0.0115690 |
| inclination: | 98.8550° |
| perigee height: | 842 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 155.7497° |
| argument of perigee: | 220.1768° |
| revolutions per day: | 13.90434698 |
| mean anomaly at epoch: | 139.0796° |
| orbit number at epoch: | 32571 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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