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 53568U 26145.50577808 +.00000000 +00000-0 +37778-3 0 00003
2 53568 53.2138 69.1481 0001462 92.2899 267.8261 15.08835309 06
| Epoch (UTC): | 25 May 2026 12:08:19 |
| Eccentricity: | 0.0001462 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 69.1481° |
| argument of perigee: | 92.2899° |
| revolutions per day: | 15.08835309 |
| mean anomaly at epoch: | 267.8261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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