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 40611U 95015FJ 24356.00344038 .00008839 00000-0 33800-2 0 9998
2 40611 98.8086 13.3836 0030630 290.2737 69.5153 14.30636144504324
| Epoch (UTC): | 21 December 2024 00:04:57 |
| Eccentricity: | 0.0030630 |
| inclination: | 98.8086° |
| perigee height: | 767 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 13.3836° |
| argument of perigee: | 290.2737° |
| revolutions per day: | 14.30636144 |
| mean anomaly at epoch: | 69.5153° |
| orbit number at epoch: | 50432 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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