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 42809U 26145.54364453 +.00000000 +00000-0 +12518-4 0 00009
2 42809 86.3986 3.1108 0002308 86.5484 273.5976 14.34217115 04
| Epoch (UTC): | 25 May 2026 13:02:50 |
| Eccentricity: | 0.0002308 |
| inclination: | 86.3986° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 3.1108° |
| argument of perigee: | 86.5484° |
| revolutions per day: | 14.34217115 |
| mean anomaly at epoch: | 273.5976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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