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 61564U 26104.58428478 +.00000000 +00000-0 -74151-4 0 00007
2 61564 88.9774 67.7678 0008527 42.6720 317.5096 13.58018562 01
| Epoch (UTC): | 14 April 2026 14:01:22 |
| Eccentricity: | 0.0008527 |
| inclination: | 88.9774° |
| perigee height: | 1037 km |
| apogee height: | 1049 km |
| right ascension of ascending node: | 67.7678° |
| argument of perigee: | 42.6720° |
| revolutions per day: | 13.58018562 |
| mean anomaly at epoch: | 317.5096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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