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 27875U 26143.94864865 +.00000000 +00000-0 +00000-0 0 00008
2 27875 10.4521 48.1798 0001818 3.4668 195.5313 1.00274024 03
| Epoch (UTC): | 23 May 2026 22:46:03 |
| Eccentricity: | 0.0001818 |
| inclination: | 10.4521° |
| perigee height: | 35778 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 48.1798° |
| argument of perigee: | 3.4668° |
| revolutions per day: | 1.00274024 |
| mean anomaly at epoch: | 195.5313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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