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 27006U 26106.68949623 +.00000000 +00000-0 +56246-5 0 00008
2 27006 99.7740 273.2063 0013798 248.4483 122.4012 13.71093426 05
| Epoch (UTC): | 16 April 2026 16:32:52 |
| Eccentricity: | 0.0013798 |
| inclination: | 99.7740° |
| perigee height: | 985 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 273.2063° |
| argument of perigee: | 248.4483° |
| revolutions per day: | 13.71093426 |
| mean anomaly at epoch: | 122.4012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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