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 64126U 26145.60276878 +.00000000 +00000-0 +13487-2 0 00009
2 64126 42.9966 230.4133 0002032 254.4756 105.5887 15.70862546 01
| Epoch (UTC): | 25 May 2026 14:27:59 |
| Eccentricity: | 0.0002032 |
| inclination: | 42.9966° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 230.4133° |
| argument of perigee: | 254.4756° |
| revolutions per day: | 15.70862546 |
| mean anomaly at epoch: | 105.5887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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