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 27711U 26139.98142057 +.00000000 +00000-0 +00000-0 0 00008
2 27711 12.3087 30.0727 0101429 7.7472 345.2676 1.00273137 01
| Epoch (UTC): | 19 May 2026 23:33:14 |
| Eccentricity: | 0.0101429 |
| inclination: | 12.3087° |
| perigee height: | 35359 km |
| apogee height: | 36214 km |
| right ascension of ascending node: | 30.0727° |
| argument of perigee: | 7.7472° |
| revolutions per day: | 1.00273137 |
| mean anomaly at epoch: | 345.2676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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