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 24280.78942154 .00001938 00000-0 87061-3 0 9994
2 27844 98.6799 286.2946 0009742 173.9803 186.1494 14.23520806103698
| Epoch (UTC): | 06 October 2024 18:56:46 |
| Eccentricity: | 0.0009742 |
| inclination: | 98.6799° |
| perigee height: | 806 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 286.2946° |
| argument of perigee: | 173.9803° |
| revolutions per day: | 14.23520806 |
| mean anomaly at epoch: | 186.1494° |
| orbit number at epoch: | 10369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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