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 60453U 24146B 24357.99735827 .00000919 00000-0 23234-3 0 9992
2 60453 45.0380 132.0157 0002980 96.9212 263.1984 14.57840723 18886
| Epoch (UTC): | 22 December 2024 23:56:11 |
| Eccentricity: | 0.0002980 |
| inclination: | 45.0380° |
| perigee height: | 698 km |
| apogee height: | 702 km |
| right ascension of ascending node: | 132.0157° |
| argument of perigee: | 96.9212° |
| revolutions per day: | 14.57840723 |
| mean anomaly at epoch: | 263.1984° |
| orbit number at epoch: | 1888 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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