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 42811U 26145.39484595 +.00000000 +00000-0 -35551-5 0 00009
2 42811 86.3987 34.6776 0002079 80.0990 280.0440 14.34217689 09
| Epoch (UTC): | 25 May 2026 09:28:34 |
| Eccentricity: | 0.0002079 |
| inclination: | 86.3987° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 34.6776° |
| argument of perigee: | 80.0990° |
| revolutions per day: | 14.34217689 |
| mean anomaly at epoch: | 280.0440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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