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 42804U 26145.32799587 +.00000000 +00000-0 +50366-4 0 00003
2 42804 86.3981 3.1941 0002147 82.0410 278.1030 14.34218441 05
| Epoch (UTC): | 25 May 2026 07:52:18 |
| Eccentricity: | 0.0002147 |
| inclination: | 86.3981° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 3.1941° |
| argument of perigee: | 82.0410° |
| revolutions per day: | 14.34218441 |
| mean anomaly at epoch: | 278.1030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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