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 40057U 26101.50958906 +.00000000 +00000-0 +27745-3 0 00009
2 40057 98.2583 2.7486 0008106 125.5978 234.5999 14.97276927 07
| Epoch (UTC): | 11 April 2026 12:13:48 |
| Eccentricity: | 0.0008106 |
| inclination: | 98.2583° |
| perigee height: | 570 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 2.7486° |
| argument of perigee: | 125.5978° |
| revolutions per day: | 14.97276927 |
| mean anomaly at epoch: | 234.5999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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