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 64426U 26145.37271713 +.00000000 +00000-0 +14656-3 0 00009
2 64426 70.0006 241.1053 0003321 273.2136 86.8643 14.98337018 05
| Epoch (UTC): | 25 May 2026 08:56:42 |
| Eccentricity: | 0.0003321 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 241.1053° |
| argument of perigee: | 273.2136° |
| revolutions per day: | 14.98337018 |
| mean anomaly at epoch: | 86.8643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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