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 01646U 65082H 24357.54960004 .00002318 00000-0 32763-3 0 9995
2 01646 32.3118 23.9059 0002782 323.6213 36.4250 14.75702824140054
| Epoch (UTC): | 22 December 2024 13:11:25 |
| Eccentricity: | 0.0002782 |
| inclination: | 32.3118° |
| perigee height: | 641 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 23.9059° |
| argument of perigee: | 323.6213° |
| revolutions per day: | 14.75702824 |
| mean anomaly at epoch: | 36.4250° |
| orbit number at epoch: | 14005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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