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 59321U 26145.25371941 +.00000000 +00000-0 +77878-4 0 00004
2 59321 43.0029 114.2390 0001194 271.1232 88.9483 15.27581323 00
| Epoch (UTC): | 25 May 2026 06:05:21 |
| Eccentricity: | 0.0001194 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.2390° |
| argument of perigee: | 271.1232° |
| revolutions per day: | 15.27581323 |
| mean anomaly at epoch: | 88.9483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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