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 27831U 26109.64945699 +.00000000 +00000-0 +00000-0 0 00004
2 27831 6.7447 70.1025 0005954 316.9698 210.2268 1.00270493 08
| Epoch (UTC): | 19 April 2026 15:35:13 |
| Eccentricity: | 0.0005954 |
| inclination: | 6.7447° |
| perigee height: | 35762 km |
| apogee height: | 35812 km |
| right ascension of ascending node: | 70.1025° |
| argument of perigee: | 316.9698° |
| revolutions per day: | 1.00270493 |
| mean anomaly at epoch: | 210.2268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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