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 23336.52281085 .00210805 00000-0 15601-2 0 9994
2 40912 97.3932 0.0406 0005519 146.0877 214.0740 15.72290111455757
| Epoch (UTC): | 02 December 2023 12:32:50 |
| Eccentricity: | 0.0005519 |
| inclination: | 97.3932° |
| perigee height: | 348 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 0.0406° |
| argument of perigee: | 146.0877° |
| revolutions per day: | 15.72290111 |
| mean anomaly at epoch: | 214.0740° |
| orbit number at epoch: | 45575 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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