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 30606U 99025AMM 24358.02942765 .00004879 00000-0 83296-3 0 9996
2 30606 98.1116 12.1482 0223690 159.8685 231.4736 14.54223548941193
| Epoch (UTC): | 23 December 2024 00:42:22 |
| Eccentricity: | 0.0223690 |
| inclination: | 98.1116° |
| perigee height: | 553 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 12.1482° |
| argument of perigee: | 159.8685° |
| revolutions per day: | 14.54223548 |
| mean anomaly at epoch: | 231.4736° |
| orbit number at epoch: | 94119 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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