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 64459U 26145.10594919 +.00000000 +00000-0 +10523-2 0 00000
2 64459 53.1601 92.8180 0001228 100.4966 259.6175 15.34412770 02
| Epoch (UTC): | 25 May 2026 02:32:34 |
| Eccentricity: | 0.0001228 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 92.8180° |
| argument of perigee: | 100.4966° |
| revolutions per day: | 15.34412770 |
| mean anomaly at epoch: | 259.6175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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