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 47739U 26145.51466801 +.00000000 +00000-0 +77863-4 0 00007
2 47739 53.1575 221.8915 0001109 89.0058 271.1070 15.31707687 00
| Epoch (UTC): | 25 May 2026 12:21:07 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.1575° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 221.8915° |
| argument of perigee: | 89.0058° |
| revolutions per day: | 15.31707687 |
| mean anomaly at epoch: | 271.1070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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