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 40024U 14033Q 23334.87023824 .00011138 00000-0 92731-3 0 9999
2 40024 98.0516 294.6688 0011977 83.2494 277.0091 14.98783580513872
| Epoch (UTC): | 30 November 2023 20:53:08 |
| Eccentricity: | 0.0011977 |
| inclination: | 98.0516° |
| perigee height: | 562 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 294.6688° |
| argument of perigee: | 83.2494° |
| revolutions per day: | 14.98783580 |
| mean anomaly at epoch: | 277.0091° |
| orbit number at epoch: | 51387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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