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 64361U 26145.41397925 +.00000000 +00000-0 +20239-3 0 00000
2 64361 70.0008 201.0368 0003890 267.1574 92.9140 14.98334886 08
| Epoch (UTC): | 25 May 2026 09:56:07 |
| Eccentricity: | 0.0003890 |
| inclination: | 70.0008° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 201.0368° |
| argument of perigee: | 267.1574° |
| revolutions per day: | 14.98334886 |
| mean anomaly at epoch: | 92.9140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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