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 24287.38344592 .00004037 00000-0 10053-2 0 9996
2 36416 63.3974 264.7999 0645286 359.5003 0.5317 13.71226308730623
| Epoch (UTC): | 13 October 2024 09:12:09 |
| Eccentricity: | 0.0645286 |
| inclination: | 63.3974° |
| perigee height: | 519 km |
| apogee height: | 1471 km |
| right ascension of ascending node: | 264.7999° |
| argument of perigee: | 359.5003° |
| revolutions per day: | 13.71226308 |
| mean anomaly at epoch: | 0.5317° |
| orbit number at epoch: | 73062 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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