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 57842U 26145.66668980 +.00000000 +00000-0 +12929-4 0 00003
2 57842 53.1585 286.4955 0001163 82.2936 230.3591 15.31692787 07
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001163 |
| inclination: | 53.1585° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 286.4955° |
| argument of perigee: | 82.2936° |
| revolutions per day: | 15.31692787 |
| mean anomaly at epoch: | 230.3591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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