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 12889U 81100C 24277.00652714 .00001862 00000-0 91838-3 0 9994
2 12889 99.8729 251.4215 1311653 87.6082 327.2399 12.19215319905705
| Epoch (UTC): | 03 October 2024 00:09:23 |
| Eccentricity: | 0.1311653 |
| inclination: | 99.8729° |
| perigee height: | 550 km |
| apogee height: | 2642 km |
| right ascension of ascending node: | 251.4215° |
| argument of perigee: | 87.6082° |
| revolutions per day: | 12.19215319 |
| mean anomaly at epoch: | 327.2399° |
| orbit number at epoch: | 90570 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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