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 28480U 04046B 23342.50132340 .00000265 00000-0 11440-3 0 9994
2 28480 98.1381 294.8610 0142222 66.5105 295.0950 14.26176500991269
| Epoch (UTC): | 08 December 2023 12:01:54 |
| Eccentricity: | 0.0142222 |
| inclination: | 98.1381° |
| perigee height: | 702 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 294.8610° |
| argument of perigee: | 66.5105° |
| revolutions per day: | 14.26176500 |
| mean anomaly at epoch: | 295.0950° |
| orbit number at epoch: | 99126 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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