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 64910U 25157G 25344.20551493 .00052397 00000-0 13092-2 0 9990
2 64910 53.1570 45.5605 0001541 60.6934 299.4225 15.39659406 22361
| Epoch (UTC): | 10 December 2025 04:55:56 |
| Eccentricity: | 0.0001541 |
| inclination: | 53.1570° |
| perigee height: | 446 km |
| apogee height: | 448 km |
| right ascension of ascending node: | 45.5605° |
| argument of perigee: | 60.6934° |
| revolutions per day: | 15.39659406 |
| mean anomaly at epoch: | 299.4225° |
| orbit number at epoch: | 2236 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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