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 64044U 26145.42743174 +.00000000 +00000-0 +13259-3 0 00004
2 64044 70.0009 281.0939 0002326 269.7754 90.3138 14.98337931 03
| Epoch (UTC): | 25 May 2026 10:15:30 |
| Eccentricity: | 0.0002326 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.0939° |
| argument of perigee: | 269.7754° |
| revolutions per day: | 14.98337931 |
| mean anomaly at epoch: | 90.3138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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