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 40302U 14070E 24279.48420010 .00455699 00000-0 21315-2 0 9996
2 40302 97.0987 287.1182 0012565 82.6606 277.6091 15.81990696550485
| Epoch (UTC): | 05 October 2024 11:37:14 |
| Eccentricity: | 0.0012565 |
| inclination: | 97.0987° |
| perigee height: | 316 km |
| apogee height: | 333 km |
| right ascension of ascending node: | 287.1182° |
| argument of perigee: | 82.6606° |
| revolutions per day: | 15.81990696 |
| mean anomaly at epoch: | 277.6091° |
| orbit number at epoch: | 55048 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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