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 47808U 26145.00747808 +.00000000 +00000-0 -35480-4 0 00007
2 47808 53.1579 247.6907 0000379 77.2680 282.8364 15.31698983 09
| Epoch (UTC): | 25 May 2026 00:10:46 |
| Eccentricity: | 0.0000379 |
| inclination: | 53.1579° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 247.6907° |
| argument of perigee: | 77.2680° |
| revolutions per day: | 15.31698983 |
| mean anomaly at epoch: | 282.8364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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