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 23091.10457608 .00010514 00000-0 96954-3 0 9994
2 40024 98.0207 44.3972 0011052 167.0072 193.1435 14.94815449477417
| Epoch (UTC): | 01 April 2023 02:30:35 |
| Eccentricity: | 0.0011052 |
| inclination: | 98.0207° |
| perigee height: | 575 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 44.3972° |
| argument of perigee: | 167.0072° |
| revolutions per day: | 14.94815449 |
| mean anomaly at epoch: | 193.1435° |
| orbit number at epoch: | 47741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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