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 46079U 26145.29467362 +.00000000 +00000-0 -23237-3 0 00007
2 46079 53.1598 104.8459 0001085 72.8836 287.2284 15.31675389 09
| Epoch (UTC): | 25 May 2026 07:04:19 |
| Eccentricity: | 0.0001085 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 104.8459° |
| argument of perigee: | 72.8836° |
| revolutions per day: | 15.31675389 |
| mean anomaly at epoch: | 287.2284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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