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 59436U 26145.11912027 +.00000000 +00000-0 +32283-3 0 00002
2 59436 53.1610 286.4862 0001528 84.4399 275.6776 15.30160891 08
| Epoch (UTC): | 25 May 2026 02:51:31 |
| Eccentricity: | 0.0001528 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 286.4862° |
| argument of perigee: | 84.4399° |
| revolutions per day: | 15.30160891 |
| mean anomaly at epoch: | 275.6776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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