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 47638U 26145.55191808 +.00000000 +00000-0 +13224-2 0 00000
2 47638 53.1580 334.8366 0002021 232.9305 127.1513 15.33697604 08
| Epoch (UTC): | 25 May 2026 13:14:45 |
| Eccentricity: | 0.0002021 |
| inclination: | 53.1580° |
| perigee height: | 463 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 334.8366° |
| argument of perigee: | 232.9305° |
| revolutions per day: | 15.33697604 |
| mean anomaly at epoch: | 127.1513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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