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 64409U 16053AP 25341.16298940 -.00000228 00000-0 00000-0 0 9995
2 64409 1.0282 79.3109 0053816 77.2435 281.9613 0.99468906 3956
| Epoch (UTC): | 07 December 2025 03:54:42 |
| Eccentricity: | 0.0053816 |
| inclination: | 1.0282° |
| perigee height: | 35784 km |
| apogee height: | 36241 km |
| right ascension of ascending node: | 79.3109° |
| argument of perigee: | 77.2435° |
| revolutions per day: | 0.99468906 |
| mean anomaly at epoch: | 281.9613° |
| orbit number at epoch: | 395 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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