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 08366U 75100A 23083.59298000 -.00000131 00000-0 00000-0 0 9991
2 08366 7.5937 292.2020 0000858 332.7206 30.0059 1.00227613173232
| Epoch (UTC): | 24 March 2023 14:13:53 |
| Eccentricity: | 0.0000858 |
| inclination: | 7.5937° |
| perigee height: | 35795 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 292.2020° |
| argument of perigee: | 332.7206° |
| revolutions per day: | 1.00227613 |
| mean anomaly at epoch: | 30.0059° |
| orbit number at epoch: | 17323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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