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 40058U 14034F 24358.09980529 .00002633 00000-0 33296-3 0 9993
2 40058 98.3300 186.5855 0019658 282.1387 77.7622 14.82655945565871
| Epoch (UTC): | 23 December 2024 02:23:43 |
| Eccentricity: | 0.0019658 |
| inclination: | 98.3300° |
| perigee height: | 607 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 186.5855° |
| argument of perigee: | 282.1387° |
| revolutions per day: | 14.82655945 |
| mean anomaly at epoch: | 77.7622° |
| orbit number at epoch: | 56587 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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