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 53727U 26145.06419019 +.00000000 +00000-0 +38550-4 0 00000
2 53727 53.2145 271.2538 0001237 92.9582 267.1551 15.08833538 03
| Epoch (UTC): | 25 May 2026 01:32:26 |
| Eccentricity: | 0.0001237 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 271.2538° |
| argument of perigee: | 92.9582° |
| revolutions per day: | 15.08833538 |
| mean anomaly at epoch: | 267.1551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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