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 data is extracted from the following two-line orbital elements,
1 27006U 01056F 23342.40494873 -.00000015 00000-0 34776-4 0 9998
2 27006 99.6559 123.4044 0013835 303.5681 117.7763 13.71011382100510
| Epoch (UTC): | 08 December 2023 09:43:07 |
| Eccentricity: | 0.0013835 |
| inclination: | 99.6559° |
| perigee height: | 986 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 123.4044° |
| argument of perigee: | 303.5681° |
| revolutions per day: | 13.71011382 |
| mean anomaly at epoch: | 117.7763° |
| orbit number at epoch: | 10051 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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