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 47728U 26145.41796272 +.00000000 +00000-0 +11229-2 0 00004
2 47728 53.0727 201.9933 0006529 1.2620 358.8402 15.45410859 06
| Epoch (UTC): | 25 May 2026 10:01:51 |
| Eccentricity: | 0.0006529 |
| inclination: | 53.0727° |
| perigee height: | 426 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 201.9933° |
| argument of perigee: | 1.2620° |
| revolutions per day: | 15.45410859 |
| mean anomaly at epoch: | 358.8402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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