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 62058U 26145.13442257 +.00000000 +00000-0 +11601-2 0 00001
2 62058 53.1570 54.1495 0000876 85.9191 274.1927 15.69733381 04
| Epoch (UTC): | 25 May 2026 03:13:34 |
| Eccentricity: | 0.0000876 |
| inclination: | 53.1570° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 54.1495° |
| argument of perigee: | 85.9191° |
| revolutions per day: | 15.69733381 |
| mean anomaly at epoch: | 274.1927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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