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 62075U 26145.53132324 +.00000000 +00000-0 +35207-3 0 00004
2 62075 53.1575 184.3700 0000956 86.1583 273.9527 15.30208870 01
| Epoch (UTC): | 25 May 2026 12:45:06 |
| Eccentricity: | 0.0000956 |
| inclination: | 53.1575° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.3700° |
| argument of perigee: | 86.1583° |
| revolutions per day: | 15.30208870 |
| mean anomaly at epoch: | 273.9527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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