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 55670U 26145.51353491 +.00000000 +00000-0 +16752-4 0 00000
2 55670 69.9988 330.6886 0002550 270.1237 89.9630 14.98330734 09
| Epoch (UTC): | 25 May 2026 12:19:29 |
| Eccentricity: | 0.0002550 |
| inclination: | 69.9988° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.6886° |
| argument of perigee: | 270.1237° |
| revolutions per day: | 14.98330734 |
| mean anomaly at epoch: | 89.9630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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