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 is defined by the following mean orbital elements,
1 46557U 26145.28414375 +.00000000 +00000-0 +80557-3 0 00000
2 46557 53.0397 107.4939 0008090 70.0785 290.1103 15.73174013 01
| Epoch (UTC): | 25 May 2026 06:49:10 |
| Eccentricity: | 0.0008090 |
| inclination: | 53.0397° |
| perigee height: | 344 km |
| apogee height: | 355 km |
| right ascension of ascending node: | 107.4939° |
| argument of perigee: | 70.0785° |
| revolutions per day: | 15.73174013 |
| mean anomaly at epoch: | 290.1103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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