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 40719U 15032E 24358.04690787 .00014749 00000-0 14430-2 0 9994
2 40719 97.6613 215.7523 0010537 230.3096 129.7195 14.92375593510209
| Epoch (UTC): | 23 December 2024 01:07:32 |
| Eccentricity: | 0.0010537 |
| inclination: | 97.6613° |
| perigee height: | 583 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 215.7523° |
| argument of perigee: | 230.3096° |
| revolutions per day: | 14.92375593 |
| mean anomaly at epoch: | 129.7195° |
| orbit number at epoch: | 51020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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