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 56464U 26145.43402299 +.00000000 +00000-0 -63770-4 0 00007
2 56464 69.9993 310.8720 0003072 270.3595 89.7212 14.98324801 05
| Epoch (UTC): | 25 May 2026 10:24:59 |
| Eccentricity: | 0.0003072 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.8720° |
| argument of perigee: | 270.3595° |
| revolutions per day: | 14.98324801 |
| mean anomaly at epoch: | 89.7212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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