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 23936U 96029E 23087.77657235 0.00002700 00000-0 71477-3 0 02
2 23936 63.3404 13.1839 0784598 32.9395 327.0605 13.41589355 09
| Epoch (UTC): | 28 March 2023 18:38:15 |
| Eccentricity: | 0.0784598 |
| inclination: | 63.3404° |
| perigee height: | 516 km |
| apogee height: | 1690 km |
| right ascension of ascending node: | 13.1839° |
| argument of perigee: | 32.9395° |
| revolutions per day: | 13.41589355 |
| mean anomaly at epoch: | 327.0605° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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