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 36416U 10009D 24281.69500780 .00004319 00000-0 10769-2 0 9994
2 36416 63.3981 280.2019 0644843 359.4632 0.5642 13.71176420729844
| Epoch (UTC): | 07 October 2024 16:40:48 |
| Eccentricity: | 0.0644843 |
| inclination: | 63.3981° |
| perigee height: | 520 km |
| apogee height: | 1471 km |
| right ascension of ascending node: | 280.2019° |
| argument of perigee: | 359.4632° |
| revolutions per day: | 13.71176420 |
| mean anomaly at epoch: | 0.5642° |
| orbit number at epoch: | 72984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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