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 26144.79797279 +.00000000 +00000-0 +68939-4 0 00007
2 27606 64.5545 322.3639 0087311 274.5121 84.6012 14.76987621 04
| Epoch (UTC): | 24 May 2026 19:09:04 |
| Eccentricity: | 0.0087311 |
| inclination: | 64.5545° |
| perigee height: | 578 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 322.3639° |
| argument of perigee: | 274.5121° |
| revolutions per day: | 14.76987621 |
| mean anomaly at epoch: | 84.6012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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