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 39241U 26145.57808549 +.00000000 +00000-0 +13060-3 0 00009
2 39241 63.3848 147.9748 0425284 11.3763 349.6516 13.45475925 08
| Epoch (UTC): | 25 May 2026 13:52:26 |
| Eccentricity: | 0.0425284 |
| inclination: | 63.3848° |
| perigee height: | 771 km |
| apogee height: | 1407 km |
| right ascension of ascending node: | 147.9748° |
| argument of perigee: | 11.3763° |
| revolutions per day: | 13.45475925 |
| mean anomaly at epoch: | 349.6516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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