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 40907U 15049J 23340.79446987 .00018991 00000-0 54963-3 0 9993
2 40907 97.4881 350.2873 0006722 263.1092 96.9386 15.35624232454903
| Epoch (UTC): | 06 December 2023 19:04:02 |
| Eccentricity: | 0.0006722 |
| inclination: | 97.4881° |
| perigee height: | 454 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 350.2873° |
| argument of perigee: | 263.1092° |
| revolutions per day: | 15.35624232 |
| mean anomaly at epoch: | 96.9386° |
| orbit number at epoch: | 45490 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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