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 12849U 81094B 23031.49104662 .00002071 00000-0 19379-3 0 9999
2 12849 82.4924 28.7910 0893650 286.4245 64.0579 13.52131615 19250
| Epoch (UTC): | 31 January 2023 11:47:06 |
| Eccentricity: | 0.0893650 |
| inclination: | 82.4924° |
| perigee height: | 399 km |
| apogee height: | 1729 km |
| right ascension of ascending node: | 28.7910° |
| argument of perigee: | 286.4245° |
| revolutions per day: | 13.52131615 |
| mean anomaly at epoch: | 64.0579° |
| orbit number at epoch: | 1925 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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