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 53930U 26145.66668980 +.00000000 +00000-0 +52650-2 0 00000
2 53930 53.2266 304.1703 0000915 58.6836 188.8899 15.61310869 06
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000915 |
| inclination: | 53.2266° |
| perigee height: | 383 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 304.1703° |
| argument of perigee: | 58.6836° |
| revolutions per day: | 15.61310869 |
| mean anomaly at epoch: | 188.8899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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