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 40930U 26145.15090551 +.00000000 +00000-0 +10243-3 0 00006
2 40930 5.9989 321.1626 0007589 63.2978 296.7926 14.82459854 04
| Epoch (UTC): | 25 May 2026 03:37:18 |
| Eccentricity: | 0.0007589 |
| inclination: | 5.9989° |
| perigee height: | 616 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 321.1626° |
| argument of perigee: | 63.2978° |
| revolutions per day: | 14.82459854 |
| mean anomaly at epoch: | 296.7926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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