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 40059U 26145.56303699 +.00000000 +00000-0 +83993-4 0 00006
2 40059 98.2011 87.2023 0001423 88.0919 272.0443 14.57088798 07
| Epoch (UTC): | 25 May 2026 13:30:46 |
| Eccentricity: | 0.0001423 |
| inclination: | 98.2011° |
| perigee height: | 702 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 87.2023° |
| argument of perigee: | 88.0919° |
| revolutions per day: | 14.57088798 |
| mean anomaly at epoch: | 272.0443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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