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 47771U 26145.45000593 +.00000000 +00000-0 +30527-4 0 00004
2 47771 53.1594 206.8317 0001275 90.7713 269.3434 15.31701913 06
| Epoch (UTC): | 25 May 2026 10:48:00 |
| Eccentricity: | 0.0001275 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 206.8317° |
| argument of perigee: | 90.7713° |
| revolutions per day: | 15.31701913 |
| mean anomaly at epoch: | 269.3434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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