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 24287.40567598 .00000066 00000-0 12480-3 0 9994
2 27006 99.7042 75.5807 0014019 221.1527 193.1989 13.71047362142994
| Epoch (UTC): | 13 October 2024 09:44:10 |
| Eccentricity: | 0.0014019 |
| inclination: | 99.7042° |
| perigee height: | 985 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 75.5807° |
| argument of perigee: | 221.1527° |
| revolutions per day: | 13.71047362 |
| mean anomaly at epoch: | 193.1989° |
| orbit number at epoch: | 14299 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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