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 62792U 26145.57116949 +.00000000 +00000-0 +13405-3 0 00005
2 62792 88.9727 86.1050 0014067 225.4282 134.5722 13.51010824 01
| Epoch (UTC): | 25 May 2026 13:42:29 |
| Eccentricity: | 0.0014067 |
| inclination: | 88.9727° |
| perigee height: | 1058 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 86.1050° |
| argument of perigee: | 225.4282° |
| revolutions per day: | 13.51010824 |
| mean anomaly at epoch: | 134.5722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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