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 56057U 26145.25618807 +.00000000 +00000-0 +13159-3 0 00003
2 56057 87.9109 233.3236 0002499 110.5220 249.6179 13.16595581 08
| Epoch (UTC): | 25 May 2026 06:08:54 |
| Eccentricity: | 0.0002499 |
| inclination: | 87.9109° |
| perigee height: | 1196 km |
| apogee height: | 1200 km |
| right ascension of ascending node: | 233.3236° |
| argument of perigee: | 110.5220° |
| revolutions per day: | 13.16595581 |
| mean anomaly at epoch: | 249.6179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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