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 64297U 26145.30751757 +.00000000 +00000-0 +19437-3 0 00001
2 64297 70.0020 1.3324 0002705 272.5248 87.5602 14.98346100 00
| Epoch (UTC): | 25 May 2026 07:22:49 |
| Eccentricity: | 0.0002705 |
| inclination: | 70.0020° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.3324° |
| argument of perigee: | 272.5248° |
| revolutions per day: | 14.98346100 |
| mean anomaly at epoch: | 87.5602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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