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 27606U 26145.47506189 +.00000000 +00000-0 +80992-4 0 00004
2 27606 64.5545 320.2889 0087313 274.3769 84.7362 14.76988839 07
| Epoch (UTC): | 25 May 2026 11:24:05 |
| Eccentricity: | 0.0087313 |
| inclination: | 64.5545° |
| perigee height: | 578 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 320.2889° |
| argument of perigee: | 274.3769° |
| revolutions per day: | 14.76988839 |
| mean anomaly at epoch: | 84.7362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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