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 58947U 26145.18733642 +.00000000 +00000-0 +60691-4 0 00004
2 58947 53.1597 314.0725 0001309 90.5652 269.5499 15.31708390 08
| Epoch (UTC): | 25 May 2026 04:29:45 |
| Eccentricity: | 0.0001309 |
| inclination: | 53.1597° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 314.0725° |
| argument of perigee: | 90.5652° |
| revolutions per day: | 15.31708390 |
| mean anomaly at epoch: | 269.5499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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