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 53572U 26145.48736435 +.00000000 +00000-0 +47779-3 0 00000
2 53572 53.2123 69.0364 0001483 93.9769 266.1392 15.08792092 09
| Epoch (UTC): | 25 May 2026 11:41:48 |
| Eccentricity: | 0.0001483 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 69.0364° |
| argument of perigee: | 93.9769° |
| revolutions per day: | 15.08792092 |
| mean anomaly at epoch: | 266.1392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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