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 40376U 15003A 24276.92558056 .00003915 00000-0 76514-3 0 9994
2 40376 98.1305 281.8047 0001859 90.0875 270.0540 14.63442773516618
| Epoch (UTC): | 02 October 2024 22:12:50 |
| Eccentricity: | 0.0001859 |
| inclination: | 98.1305° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 281.8047° |
| argument of perigee: | 90.0875° |
| revolutions per day: | 14.63442773 |
| mean anomaly at epoch: | 270.0540° |
| orbit number at epoch: | 51661 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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