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 64369U 26145.43084112 +.00000000 +00000-0 +25540-3 0 00001
2 64369 70.0007 201.0915 0003746 267.5015 92.5715 14.98336177 06
| Epoch (UTC): | 25 May 2026 10:20:24 |
| Eccentricity: | 0.0003746 |
| inclination: | 70.0007° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 201.0915° |
| argument of perigee: | 267.5015° |
| revolutions per day: | 14.98336177 |
| mean anomaly at epoch: | 92.5715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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