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 24181.51780098 .07500886 23432-5 86307-3 0 9999
2 42778 97.0566 220.7984 0007714 249.3707 110.6764 16.36858806391577
| Epoch (UTC): | 29 June 2024 12:25:38 |
| Eccentricity: | 0.0007714 |
| inclination: | 97.0566° |
| perigee height: | 169 km |
| apogee height: | 179 km |
| right ascension of ascending node: | 220.7984° |
| argument of perigee: | 249.3707° |
| revolutions per day: | 16.36858806 |
| mean anomaly at epoch: | 110.6764° |
| orbit number at epoch: | 39157 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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