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 64796U 26145.39027376 +.00000000 +00000-0 +21773-3 0 00003
2 64796 70.0006 301.1476 0002736 263.7566 96.3281 14.98337151 03
| Epoch (UTC): | 25 May 2026 09:21:59 |
| Eccentricity: | 0.0002736 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 301.1476° |
| argument of perigee: | 263.7566° |
| revolutions per day: | 14.98337151 |
| mean anomaly at epoch: | 96.3281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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