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 64795U 26145.41512664 +.00000000 +00000-0 +29665-3 0 00002
2 64795 70.0015 300.8393 0002523 264.5814 95.5057 14.98336520 06
| Epoch (UTC): | 25 May 2026 09:57:46 |
| Eccentricity: | 0.0002523 |
| inclination: | 70.0015° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.8393° |
| argument of perigee: | 264.5814° |
| revolutions per day: | 14.98336520 |
| mean anomaly at epoch: | 95.5057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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