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 27844U 03031E 24340.46041004 .00001088 00000-0 49582-3 0 9992
2 27844 98.6781 345.1636 0009948 14.2846 345.8612 14.23683881112152
| Epoch (UTC): | 05 December 2024 11:02:59 |
| Eccentricity: | 0.0009948 |
| inclination: | 98.6781° |
| perigee height: | 806 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 345.1636° |
| argument of perigee: | 14.2846° |
| revolutions per day: | 14.23683881 |
| mean anomaly at epoch: | 345.8612° |
| orbit number at epoch: | 11215 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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