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 28380U 04028A 23341.56788583 .00000071 00000-0 56890-4 0 9998
2 28380 82.9623 38.0331 0038146 314.0840 155.6843 13.76181583972961
| Epoch (UTC): | 07 December 2023 13:37:45 |
| Eccentricity: | 0.0038146 |
| inclination: | 82.9623° |
| perigee height: | 949 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 38.0331° |
| argument of perigee: | 314.0840° |
| revolutions per day: | 13.76181583 |
| mean anomaly at epoch: | 155.6843° |
| orbit number at epoch: | 97296 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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