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 58397U 70047D 24251.79211284 .00002690 00000-0 13709-2 0 9997
2 58397 81.2187 154.6801 0031369 99.5447 260.9274 14.15249798 44824
| Epoch (UTC): | 07 September 2024 19:00:38 |
| Eccentricity: | 0.0031369 |
| inclination: | 81.2187° |
| perigee height: | 819 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 154.6801° |
| argument of perigee: | 99.5447° |
| revolutions per day: | 14.15249798 |
| mean anomaly at epoch: | 260.9274° |
| orbit number at epoch: | 4482 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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