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 27811U 26145.58173508 +.00000000 +00000-0 +00000-0 0 00007
2 27811 7.3013 68.1521 0003065 337.0448 37.3849 1.00271827 03
| Epoch (UTC): | 25 May 2026 13:57:41 |
| Eccentricity: | 0.0003065 |
| inclination: | 7.3013° |
| perigee height: | 35774 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 68.1521° |
| argument of perigee: | 337.0448° |
| revolutions per day: | 1.00271827 |
| mean anomaly at epoch: | 37.3849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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