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 59011U 26145.53735872 +.00000000 +00000-0 -46548-4 0 00009
2 59011 53.1605 81.5536 0000953 88.1659 271.9451 15.30180906 02
| Epoch (UTC): | 25 May 2026 12:53:47 |
| Eccentricity: | 0.0000953 |
| inclination: | 53.1605° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 81.5536° |
| argument of perigee: | 88.1659° |
| revolutions per day: | 15.30180906 |
| mean anomaly at epoch: | 271.9451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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