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 46557U 20070AB 25345.88154941 .00058287 00000-0 16274-2 0 9997
2 46557 53.0544 183.9130 0011807 138.9477 221.2415 15.36123677286645
| Epoch (UTC): | 11 December 2025 21:09:25 |
| Eccentricity: | 0.0011807 |
| inclination: | 53.0544° |
| perigee height: | 449 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 183.9130° |
| argument of perigee: | 138.9477° |
| revolutions per day: | 15.36123677 |
| mean anomaly at epoch: | 221.2415° |
| orbit number at epoch: | 28664 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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