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 53773U 26145.44045644 +.00000000 +00000-0 +33578-4 0 00007
2 53773 53.2163 299.4945 0001303 90.6611 269.4530 15.08840546 09
| Epoch (UTC): | 25 May 2026 10:34:15 |
| Eccentricity: | 0.0001303 |
| inclination: | 53.2163° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 299.4945° |
| argument of perigee: | 90.6611° |
| revolutions per day: | 15.08840546 |
| mean anomaly at epoch: | 269.4530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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