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 24259.90638784 .00011026 00000-0 75510-3 0 9998
2 40014 98.1172 306.1563 0034587 186.9624 173.1126 15.05772955559282
| Epoch (UTC): | 15 September 2024 21:45:11 |
| Eccentricity: | 0.0034587 |
| inclination: | 98.1172° |
| perigee height: | 525 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 306.1563° |
| argument of perigee: | 186.9624° |
| revolutions per day: | 15.05772955 |
| mean anomaly at epoch: | 173.1126° |
| orbit number at epoch: | 55928 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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