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 56493U 26145.38743666 +.00000000 +00000-0 +28583-4 0 00001
2 56493 69.9993 251.0833 0003131 270.0745 90.0055 14.98331937 06
| Epoch (UTC): | 25 May 2026 09:17:54 |
| Eccentricity: | 0.0003131 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 251.0833° |
| argument of perigee: | 270.0745° |
| revolutions per day: | 14.98331937 |
| mean anomaly at epoch: | 90.0055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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