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 42778U 17036P 23148.06754550 .00016622 00000-0 44646-3 0 9999
2 42778 97.1573 183.3981 0009565 160.6829 199.4781 15.37947208329630
| Epoch (UTC): | 28 May 2023 01:37:15 |
| Eccentricity: | 0.0009565 |
| inclination: | 97.1573° |
| perigee height: | 445 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 183.3981° |
| argument of perigee: | 160.6829° |
| revolutions per day: | 15.37947208 |
| mean anomaly at epoch: | 199.4781° |
| orbit number at epoch: | 32963 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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