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 64324U 26145.41358872 +.00000000 +00000-0 +15669-2 0 00007
2 64324 42.9955 286.5150 0001644 287.6265 72.4424 15.70900234 07
| Epoch (UTC): | 25 May 2026 09:55:34 |
| Eccentricity: | 0.0001644 |
| inclination: | 42.9955° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 286.5150° |
| argument of perigee: | 287.6265° |
| revolutions per day: | 15.70900234 |
| mean anomaly at epoch: | 72.4424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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