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 26066.48612601 +.00000000 +00000-0 +54826-3 0 00005
2 40057 98.2639 325.7591 0005777 247.3439 112.7171 14.96830989 02
| Epoch (UTC): | 07 March 2026 11:40:01 |
| Eccentricity: | 0.0005777 |
| inclination: | 98.2639° |
| perigee height: | 573 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 325.7591° |
| argument of perigee: | 247.3439° |
| revolutions per day: | 14.96830989 |
| mean anomaly at epoch: | 112.7171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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