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 28420U 04037B 23083.76315851 .00000012 00000-0 16756-4 0 9994
2 28420 82.4907 348.0317 0013951 350.1888 9.8926 12.45288864840909
| Epoch (UTC): | 24 March 2023 18:18:56 |
| Eccentricity: | 0.0013951 |
| inclination: | 82.4907° |
| perigee height: | 1473 km |
| apogee height: | 1495 km |
| right ascension of ascending node: | 348.0317° |
| argument of perigee: | 350.1888° |
| revolutions per day: | 12.45288864 |
| mean anomaly at epoch: | 9.8926° |
| orbit number at epoch: | 84090 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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