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 36302U 75087C 24276.85983432 .00000570 00000-0 30014-3 0 9997
2 36302 81.2511 319.3825 0113626 74.4231 342.2240 14.09503151803237
| Epoch (UTC): | 02 October 2024 20:38:09 |
| Eccentricity: | 0.0113626 |
| inclination: | 81.2511° |
| perigee height: | 779 km |
| apogee height: | 943 km |
| right ascension of ascending node: | 319.3825° |
| argument of perigee: | 74.4231° |
| revolutions per day: | 14.09503151 |
| mean anomaly at epoch: | 342.2240° |
| orbit number at epoch: | 80323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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