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 58106U 26145.39642061 +.00000000 +00000-0 +13459-3 0 00007
2 58106 53.1601 155.7448 0000942 92.3610 267.7500 15.34394161 02
| Epoch (UTC): | 25 May 2026 09:30:50 |
| Eccentricity: | 0.0000942 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 155.7448° |
| argument of perigee: | 92.3610° |
| revolutions per day: | 15.34394161 |
| mean anomaly at epoch: | 267.7500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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