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 56781U 26145.43217902 +.00000000 +00000-0 +58848-4 0 00003
2 56781 69.9985 151.0355 0003579 267.7706 92.3043 14.98331566 01
| Epoch (UTC): | 25 May 2026 10:22:20 |
| Eccentricity: | 0.0003579 |
| inclination: | 69.9985° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 151.0355° |
| argument of perigee: | 267.7706° |
| revolutions per day: | 14.98331566 |
| mean anomaly at epoch: | 92.3043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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