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 64026U 26145.37319414 +.00000000 +00000-0 +42259-3 0 00006
2 64026 70.0004 281.3059 0003128 268.2500 91.8300 14.98338840 05
| Epoch (UTC): | 25 May 2026 08:57:23 |
| Eccentricity: | 0.0003128 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.3059° |
| argument of perigee: | 268.2500° |
| revolutions per day: | 14.98338840 |
| mean anomaly at epoch: | 91.8300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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