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 64345U 26145.58335647 +.00000000 +00000-0 +28596-2 0 00006
2 64345 70.0009 200.4847 0003685 265.4877 40.4822 14.98323145 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0003685 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.4847° |
| argument of perigee: | 265.4877° |
| revolutions per day: | 14.98323145 |
| mean anomaly at epoch: | 40.4822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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