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 26088.14316692 +.00000000 +00000-0 +78671-3 0 00007
2 40057 98.2616 348.6298 0007737 161.2553 198.8953 14.97105140 02
| Epoch (UTC): | 29 March 2026 03:26:09 |
| Eccentricity: | 0.0007737 |
| inclination: | 98.2616° |
| perigee height: | 570 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 348.6298° |
| argument of perigee: | 161.2553° |
| revolutions per day: | 14.97105140 |
| mean anomaly at epoch: | 198.8953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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