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 47555U 26145.34560353 +.00000000 +00000-0 +13299-2 0 00002
2 47555 53.0540 10.6332 0003276 94.9351 265.2026 15.38603867 09
| Epoch (UTC): | 25 May 2026 08:17:40 |
| Eccentricity: | 0.0003276 |
| inclination: | 53.0540° |
| perigee height: | 448 km |
| apogee height: | 452 km |
| right ascension of ascending node: | 10.6332° |
| argument of perigee: | 94.9351° |
| revolutions per day: | 15.38603867 |
| mean anomaly at epoch: | 265.2026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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