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 64329U 26145.39765735 +.00000000 +00000-0 +18833-2 0 00005
2 64329 42.9985 286.3858 0001159 245.8913 114.1833 15.71007156 05
| Epoch (UTC): | 25 May 2026 09:32:37 |
| Eccentricity: | 0.0001159 |
| inclination: | 42.9985° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 286.3858° |
| argument of perigee: | 245.8913° |
| revolutions per day: | 15.71007156 |
| mean anomaly at epoch: | 114.1833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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