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 47632U 26145.24435330 +.00000000 +00000-0 +38606-4 0 00004
2 47632 53.1605 336.6416 0000919 74.1542 285.9561 15.31703888 05
| Epoch (UTC): | 25 May 2026 05:51:52 |
| Eccentricity: | 0.0000919 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 336.6416° |
| argument of perigee: | 74.1542° |
| revolutions per day: | 15.31703888 |
| mean anomaly at epoch: | 285.9561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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