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 64022U 26145.33997535 +.00000000 +00000-0 +42492-3 0 00003
2 64022 70.0001 281.1939 0003313 271.1451 88.9328 14.98329483 07
| Epoch (UTC): | 25 May 2026 08:09:33 |
| Eccentricity: | 0.0003313 |
| inclination: | 70.0001° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.1939° |
| argument of perigee: | 271.1451° |
| revolutions per day: | 14.98329483 |
| mean anomaly at epoch: | 88.9328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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