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 43070U 26145.61633373 +.00000000 +00000-0 -19393-4 0 00007
2 43070 86.3951 331.4558 0002061 89.0271 271.1161 14.34217107 02
| Epoch (UTC): | 25 May 2026 14:47:31 |
| Eccentricity: | 0.0002061 |
| inclination: | 86.3951° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 331.4558° |
| argument of perigee: | 89.0271° |
| revolutions per day: | 14.34217107 |
| mean anomaly at epoch: | 271.1161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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