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 66827U 26145.38824774 +.00000000 +00000-0 +29588-3 0 00008
2 66827 70.0006 141.1119 0004060 265.4093 94.6603 14.98337561 06
| Epoch (UTC): | 25 May 2026 09:19:04 |
| Eccentricity: | 0.0004060 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.1119° |
| argument of perigee: | 265.4093° |
| revolutions per day: | 14.98337561 |
| mean anomaly at epoch: | 94.6603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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