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 47277U 26145.54403841 +.00000000 +00000-0 -61137-3 0 00009
2 47277 87.8949 355.1756 0001744 85.1816 274.9512 13.12443041 04
| Epoch (UTC): | 25 May 2026 13:03:24 |
| Eccentricity: | 0.0001744 |
| inclination: | 87.8949° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1756° |
| argument of perigee: | 85.1816° |
| revolutions per day: | 13.12443041 |
| mean anomaly at epoch: | 274.9512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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