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 42955U 26145.63586336 +.00000000 +00000-0 +31097-4 0 00000
2 42955 86.3990 34.6942 0002237 83.8748 276.2703 14.34218605 03
| Epoch (UTC): | 25 May 2026 15:15:38 |
| Eccentricity: | 0.0002237 |
| inclination: | 86.3990° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 34.6942° |
| argument of perigee: | 83.8748° |
| revolutions per day: | 14.34218605 |
| mean anomaly at epoch: | 276.2703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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