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 23332.13294068 .00010777 00000-0 89895-3 0 9991
2 40024 98.0517 291.8432 0012229 90.9938 269.2685 14.98717618512946
| Epoch (UTC): | 28 November 2023 03:11:26 |
| Eccentricity: | 0.0012229 |
| inclination: | 98.0517° |
| perigee height: | 562 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 291.8432° |
| argument of perigee: | 90.9938° |
| revolutions per day: | 14.98717618 |
| mean anomaly at epoch: | 269.2685° |
| orbit number at epoch: | 51294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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