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 64755U 26145.56622130 +.00000000 +00000-0 +11807-2 0 00002
2 64755 53.1583 244.8423 0001313 94.9806 265.1346 15.34407132 02
| Epoch (UTC): | 25 May 2026 13:35:21 |
| Eccentricity: | 0.0001313 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 244.8423° |
| argument of perigee: | 94.9806° |
| revolutions per day: | 15.34407132 |
| mean anomaly at epoch: | 265.1346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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