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 58826U 26145.41278801 +.00000000 +00000-0 +47738-4 0 00004
2 58826 53.1596 207.8988 0000906 98.2746 261.8358 15.30193711 07
| Epoch (UTC): | 25 May 2026 09:54:24 |
| Eccentricity: | 0.0000906 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.8988° |
| argument of perigee: | 98.2746° |
| revolutions per day: | 15.30193711 |
| mean anomaly at epoch: | 261.8358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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