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 32258U 26140.51338247 +.00000000 +00000-0 +00000-0 0 00009
2 32258 0.0655 94.7130 0000330 227.3002 58.4846 1.00270210 02
| Epoch (UTC): | 20 May 2026 12:19:16 |
| Eccentricity: | 0.0000330 |
| inclination: | 0.0655° |
| perigee height: | 35786 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 94.7130° |
| argument of perigee: | 227.3002° |
| revolutions per day: | 1.00270210 |
| mean anomaly at epoch: | 58.4846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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