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 56453U 26145.46741774 +.00000000 +00000-0 +57182-4 0 00001
2 56453 69.9985 310.9902 0002387 271.2166 88.8720 14.98331003 05
| Epoch (UTC): | 25 May 2026 11:13:04 |
| Eccentricity: | 0.0002387 |
| inclination: | 69.9985° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.9902° |
| argument of perigee: | 271.2166° |
| revolutions per day: | 14.98331003 |
| mean anomaly at epoch: | 88.8720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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