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 60591U 26145.47737484 +.00000000 +00000-0 +13588-3 0 00004
2 60591 53.1612 310.6578 0000989 86.6627 273.4487 15.30190623 07
| Epoch (UTC): | 25 May 2026 11:27:25 |
| Eccentricity: | 0.0000989 |
| inclination: | 53.1612° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.6578° |
| argument of perigee: | 86.6627° |
| revolutions per day: | 15.30190623 |
| mean anomaly at epoch: | 273.4487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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