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 47730U 26145.46242669 +.00000000 +00000-0 -11264-3 0 00009
2 47730 53.1586 219.8942 0001274 92.9356 267.1791 15.31689132 06
| Epoch (UTC): | 25 May 2026 11:05:53 |
| Eccentricity: | 0.0001274 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 219.8942° |
| argument of perigee: | 92.9356° |
| revolutions per day: | 15.31689132 |
| mean anomaly at epoch: | 267.1791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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