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 40972U 15058J 24357.63678835 .00038974 00000-0 20231-2 0 9999
2 40972 64.7647 83.1127 0131068 246.4982 112.2322 15.08700799 36181
| Epoch (UTC): | 22 December 2024 15:16:58 |
| Eccentricity: | 0.0131068 |
| inclination: | 64.7647° |
| perigee height: | 449 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 83.1127° |
| argument of perigee: | 246.4982° |
| revolutions per day: | 15.08700799 |
| mean anomaly at epoch: | 112.2322° |
| orbit number at epoch: | 3618 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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