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 24284.56711971 .00001858 00000-0 91707-3 0 9994
2 12889 99.8751 257.5345 1311487 72.3850 32.3463 12.19243575906409
| Epoch (UTC): | 10 October 2024 13:36:39 |
| Eccentricity: | 0.1311487 |
| inclination: | 99.8751° |
| perigee height: | 550 km |
| apogee height: | 2641 km |
| right ascension of ascending node: | 257.5345° |
| argument of perigee: | 72.3850° |
| revolutions per day: | 12.19243575 |
| mean anomaly at epoch: | 32.3463° |
| orbit number at epoch: | 90640 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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