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 27846U 03031G 24285.75544597 .00001745 00000-0 78864-3 0 9994
2 27846 98.6902 290.6978 0010096 136.6478 223.5496 14.23322571104405
| Epoch (UTC): | 11 October 2024 18:07:50 |
| Eccentricity: | 0.0010096 |
| inclination: | 98.6902° |
| perigee height: | 807 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 290.6978° |
| argument of perigee: | 136.6478° |
| revolutions per day: | 14.23322571 |
| mean anomaly at epoch: | 223.5496° |
| orbit number at epoch: | 10440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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