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 28381U 04028B 24284.55990845 .00000271 00000-0 25098-3 0 9998
2 28381 82.9578 148.4437 0033120 87.5035 334.6949 13.78495017 17080
| Epoch (UTC): | 10 October 2024 13:26:16 |
| Eccentricity: | 0.0033120 |
| inclination: | 82.9578° |
| perigee height: | 945 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 148.4437° |
| argument of perigee: | 87.5035° |
| revolutions per day: | 13.78495017 |
| mean anomaly at epoch: | 334.6949° |
| orbit number at epoch: | 1708 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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