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 60953U 98067WT 24343.67168105 .13878711 12527-4 44135-3 0 9990
2 60953 51.5977 155.7050 0005998 270.7882 89.2459 16.44564326 15911
| Epoch (UTC): | 08 December 2024 16:07:13 |
| Eccentricity: | 0.0005998 |
| inclination: | 51.5977° |
| perigee height: | 150 km |
| apogee height: | 157 km |
| right ascension of ascending node: | 155.7050° |
| argument of perigee: | 270.7882° |
| revolutions per day: | 16.44564326 |
| mean anomaly at epoch: | 89.2459° |
| orbit number at epoch: | 1591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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