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 53729U 26145.34021007 +.00000000 +00000-0 -58511-4 0 00009
2 53729 53.2151 270.1326 0000323 59.8558 300.2466 15.08828117 06
| Epoch (UTC): | 25 May 2026 08:09:54 |
| Eccentricity: | 0.0000323 |
| inclination: | 53.2151° |
| perigee height: | 540 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 270.1326° |
| argument of perigee: | 59.8558° |
| revolutions per day: | 15.08828117 |
| mean anomaly at epoch: | 300.2466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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