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 40014U 14033E 24280.83598271 .00016161 00000-0 10888-2 0 9991
2 40014 98.1118 328.1778 0035302 118.3081 242.1713 15.06254928562432
| Epoch (UTC): | 06 October 2024 20:03:48 |
| Eccentricity: | 0.0035302 |
| inclination: | 98.1118° |
| perigee height: | 523 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 328.1778° |
| argument of perigee: | 118.3081° |
| revolutions per day: | 15.06254928 |
| mean anomaly at epoch: | 242.1713° |
| orbit number at epoch: | 56243 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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