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 32706U 08010A 24129.61401806 0.00000000 00000-0 00000-0 0 04
2 32706 63.7052 58.5031 7115421 268.3134 16.5084 2.00627144 03
| Epoch (UTC): | 08 May 2024 14:44:11 |
| Eccentricity: | 0.7115421 |
| inclination: | 63.7052° |
| perigee height: | 1282 km |
| apogee height: | 39071 km |
| right ascension of ascending node: | 58.5031° |
| argument of perigee: | 268.3134° |
| revolutions per day: | 2.00627144 |
| mean anomaly at epoch: | 16.5084° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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