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 40069U 26103.24551249 +.00000000 +00000-0 +11213-3 0 00007
2 40069 98.5073 81.3014 0004805 217.2391 142.8454 14.21443513 08
| Epoch (UTC): | 13 April 2026 05:53:32 |
| Eccentricity: | 0.0004805 |
| inclination: | 98.5073° |
| perigee height: | 817 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 81.3014° |
| argument of perigee: | 217.2391° |
| revolutions per day: | 14.21443513 |
| mean anomaly at epoch: | 142.8454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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