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 24281.47621758 .00004224 00000-0 10542-2 0 9993
2 36416 63.3980 280.7942 0644818 359.4625 0.5649 13.71174271730006
| Epoch (UTC): | 07 October 2024 11:25:45 |
| Eccentricity: | 0.0644818 |
| inclination: | 63.3980° |
| perigee height: | 520 km |
| apogee height: | 1471 km |
| right ascension of ascending node: | 280.7942° |
| argument of perigee: | 359.4625° |
| revolutions per day: | 13.71174271 |
| mean anomaly at epoch: | 0.5649° |
| orbit number at epoch: | 73000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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