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 53420U 26145.37883289 +.00000000 +00000-0 -72375-5 0 00003
2 53420 53.2133 129.8482 0001323 68.8750 291.2383 15.08843869 00
| Epoch (UTC): | 25 May 2026 09:05:31 |
| Eccentricity: | 0.0001323 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 129.8482° |
| argument of perigee: | 68.8750° |
| revolutions per day: | 15.08843869 |
| mean anomaly at epoch: | 291.2383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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