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 52579U 26145.29593071 +.00000000 +00000-0 +88375-3 0 00009
2 52579 53.2167 150.2219 0001418 66.0764 294.0377 15.08942735 03
| Epoch (UTC): | 25 May 2026 07:06:08 |
| Eccentricity: | 0.0001418 |
| inclination: | 53.2167° |
| perigee height: | 538 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 150.2219° |
| argument of perigee: | 66.0764° |
| revolutions per day: | 15.08942735 |
| mean anomaly at epoch: | 294.0377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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