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 24254.63657465 .00001322 00000-0 35836-3 0 9995
2 36416 63.4018 353.4466 0642456 359.3343 0.6776 13.71063321726134
| Epoch (UTC): | 10 September 2024 15:16:40 |
| Eccentricity: | 0.0642456 |
| inclination: | 63.4018° |
| perigee height: | 522 km |
| apogee height: | 1469 km |
| right ascension of ascending node: | 353.4466° |
| argument of perigee: | 359.3343° |
| revolutions per day: | 13.71063321 |
| mean anomaly at epoch: | 0.6776° |
| orbit number at epoch: | 72613 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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