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 58936U 26145.49588811 +.00000000 +00000-0 +35755-4 0 00005
2 58936 53.1599 313.1522 0001005 82.2993 277.8122 15.30196275 09
| Epoch (UTC): | 25 May 2026 11:54:04 |
| Eccentricity: | 0.0001005 |
| inclination: | 53.1599° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.1522° |
| argument of perigee: | 82.2993° |
| revolutions per day: | 15.30196275 |
| mean anomaly at epoch: | 277.8122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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