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 64396U 16053AA 25340.71350661 -.00000216 00000-0 00000-0 0 9996
2 64396 1.0718 84.5036 0113272 59.5063 300.2578 0.98613417 4083
| Epoch (UTC): | 06 December 2025 17:07:26 |
| Eccentricity: | 0.0113272 |
| inclination: | 1.0718° |
| perigee height: | 35774 km |
| apogee height: | 36740 km |
| right ascension of ascending node: | 84.5036° |
| argument of perigee: | 59.5063° |
| revolutions per day: | 0.98613417 |
| mean anomaly at epoch: | 300.2578° |
| orbit number at epoch: | 408 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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