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 40912U 15049P 24021.57719025 .14527648 26197-5 35116-3 0 9996
2 40912 97.3681 54.2491 0008751 245.2391 114.8002 16.45639284463696
| Epoch (UTC): | 21 January 2024 13:51:09 |
| Eccentricity: | 0.0008751 |
| inclination: | 97.3681° |
| perigee height: | 145 km |
| apogee height: | 156 km |
| right ascension of ascending node: | 54.2491° |
| argument of perigee: | 245.2391° |
| revolutions per day: | 16.45639284 |
| mean anomaly at epoch: | 114.8002° |
| orbit number at epoch: | 46369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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