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 56485U 26145.66327299 +.00000000 +00000-0 +21340-4 0 00007
2 56485 69.9985 290.1935 0002743 273.6060 86.4785 14.98328356 02
| Epoch (UTC): | 25 May 2026 15:55:06 |
| Eccentricity: | 0.0002743 |
| inclination: | 69.9985° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 290.1935° |
| argument of perigee: | 273.6060° |
| revolutions per day: | 14.98328356 |
| mean anomaly at epoch: | 86.4785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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