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 40733U 26145.28466968 +.00000000 +00000-0 +00000-0 0 00007
2 40733 0.0261 6.1630 0002542 46.9371 222.2516 1.00270598 09
| Epoch (UTC): | 25 May 2026 06:49:55 |
| Eccentricity: | 0.0002542 |
| inclination: | 0.0261° |
| perigee height: | 35776 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 6.1630° |
| argument of perigee: | 46.9371° |
| revolutions per day: | 1.00270598 |
| mean anomaly at epoch: | 222.2516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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