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 47358U 26145.12293536 +.00000000 +00000-0 +15975-2 0 00008
2 47358 53.1603 41.7425 0001415 111.6336 248.4815 15.30390891 03
| Epoch (UTC): | 25 May 2026 02:57:01 |
| Eccentricity: | 0.0001415 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 41.7425° |
| argument of perigee: | 111.6336° |
| revolutions per day: | 15.30390891 |
| mean anomaly at epoch: | 248.4815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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