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 27608U 26106.29101110 +.00000000 +00000-0 +79366-4 0 00001
2 27608 64.5520 213.3033 0062925 263.3242 96.0700 14.84192401 04
| Epoch (UTC): | 16 April 2026 06:59:03 |
| Eccentricity: | 0.0062925 |
| inclination: | 64.5520° |
| perigee height: | 572 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 213.3033° |
| argument of perigee: | 263.3242° |
| revolutions per day: | 14.84192401 |
| mean anomaly at epoch: | 96.0700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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