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 59722U 26145.40650978 +.00000000 +00000-0 +15619-2 0 00009
2 59722 53.1592 143.8636 0001123 91.9311 268.1819 15.30545040 06
| Epoch (UTC): | 25 May 2026 09:45:22 |
| Eccentricity: | 0.0001123 |
| inclination: | 53.1592° |
| perigee height: | 473 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 143.8636° |
| argument of perigee: | 91.9311° |
| revolutions per day: | 15.30545040 |
| mean anomaly at epoch: | 268.1819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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