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 12727U 81053BU 24358.15356362 .00002983 00000-0 22406-2 0 9997
2 12727 83.2871 48.6899 0092515 230.9801 192.6270 13.92127802183025
| Epoch (UTC): | 23 December 2024 03:41:07 |
| Eccentricity: | 0.0092515 |
| inclination: | 83.2871° |
| perigee height: | 853 km |
| apogee height: | 989 km |
| right ascension of ascending node: | 48.6899° |
| argument of perigee: | 230.9801° |
| revolutions per day: | 13.92127802 |
| mean anomaly at epoch: | 192.6270° |
| orbit number at epoch: | 18302 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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