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 64806U 26145.41095347 +.00000000 +00000-0 +20193-3 0 00006
2 64806 70.0005 300.8210 0002469 272.9189 87.1687 14.98335405 00
| Epoch (UTC): | 25 May 2026 09:51:46 |
| Eccentricity: | 0.0002469 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.8210° |
| argument of perigee: | 272.9189° |
| revolutions per day: | 14.98335405 |
| mean anomaly at epoch: | 87.1687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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