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 42957U 26145.38850368 +.00000000 +00000-0 +13128-4 0 00008
2 42957 86.3988 34.7167 0002296 83.6010 276.5447 14.34217680 07
| Epoch (UTC): | 25 May 2026 09:19:26 |
| Eccentricity: | 0.0002296 |
| inclination: | 86.3988° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 34.7167° |
| argument of perigee: | 83.6010° |
| revolutions per day: | 14.34217680 |
| mean anomaly at epoch: | 276.5447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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