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 64681U 26145.32368808 +.00000000 +00000-0 +10579-2 0 00008
2 64681 53.1581 129.9093 0001078 89.4998 270.6128 15.34402666 09
| Epoch (UTC): | 25 May 2026 07:46:06 |
| Eccentricity: | 0.0001078 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 129.9093° |
| argument of perigee: | 89.4998° |
| revolutions per day: | 15.34402666 |
| mean anomaly at epoch: | 270.6128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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