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 46725U 26145.63717985 +.00000000 +00000-0 +57924-3 0 00001
2 46725 53.0481 221.2000 0005893 314.5037 45.5496 15.66783373 04
| Epoch (UTC): | 25 May 2026 15:17:32 |
| Eccentricity: | 0.0005893 |
| inclination: | 53.0481° |
| perigee height: | 364 km |
| apogee height: | 372 km |
| right ascension of ascending node: | 221.2000° |
| argument of perigee: | 314.5037° |
| revolutions per day: | 15.66783373 |
| mean anomaly at epoch: | 45.5496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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