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 47746U 26145.33686141 +.00000000 +00000-0 +10215-2 0 00002
2 47746 53.1572 204.0043 0005460 1.5497 358.5526 15.44855128 04
| Epoch (UTC): | 25 May 2026 08:05:04 |
| Eccentricity: | 0.0005460 |
| inclination: | 53.1572° |
| perigee height: | 428 km |
| apogee height: | 436 km |
| right ascension of ascending node: | 204.0043° |
| argument of perigee: | 1.5497° |
| revolutions per day: | 15.44855128 |
| mean anomaly at epoch: | 358.5526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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