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 47281U 26145.53048787 +.00000000 +00000-0 -11805-2 0 00003
2 47281 87.8951 355.1758 0001552 79.1774 280.9529 13.12442266 00
| Epoch (UTC): | 25 May 2026 12:43:54 |
| Eccentricity: | 0.0001552 |
| inclination: | 87.8951° |
| perigee height: | 1213 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1758° |
| argument of perigee: | 79.1774° |
| revolutions per day: | 13.12442266 |
| mean anomaly at epoch: | 280.9529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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