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 43570U 26145.48072271 +.00000000 +00000-0 +30274-4 0 00001
2 43570 86.3967 66.2400 0002151 82.3191 277.8249 14.34218107 01
| Epoch (UTC): | 25 May 2026 11:32:14 |
| Eccentricity: | 0.0002151 |
| inclination: | 86.3967° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 66.2400° |
| argument of perigee: | 82.3191° |
| revolutions per day: | 14.34218107 |
| mean anomaly at epoch: | 277.8249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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