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 40534U 26144.62808292 +.00000000 +00000-0 +00000-0 0 00003
2 40534 53.1699 205.1520 0109123 40.0333 320.8330 2.00552773 05
| Epoch (UTC): | 24 May 2026 15:04:26 |
| Eccentricity: | 0.0109123 |
| inclination: | 53.1699° |
| perigee height: | 19893 km |
| apogee height: | 20473 km |
| right ascension of ascending node: | 205.1520° |
| argument of perigee: | 40.0333° |
| revolutions per day: | 2.00552773 |
| mean anomaly at epoch: | 320.8330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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