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 58946U 26144.66068809 +.00000000 +00000-0 -19424-4 0 00000
2 58946 53.1602 316.4769 0001306 84.5294 275.5856 15.31687905 02
| Epoch (UTC): | 24 May 2026 15:51:23 |
| Eccentricity: | 0.0001306 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 316.4769° |
| argument of perigee: | 84.5294° |
| revolutions per day: | 15.31687905 |
| mean anomaly at epoch: | 275.5856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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