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 40042U 14033AJ 23340.42751030 .00008395 00000-0 71817-3 0 9997
2 40042 98.0303 293.1471 0014953 75.5121 284.7758 14.97784647513798
| Epoch (UTC): | 06 December 2023 10:15:36 |
| Eccentricity: | 0.0014953 |
| inclination: | 98.0303° |
| perigee height: | 563 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 293.1471° |
| argument of perigee: | 75.5121° |
| revolutions per day: | 14.97784647 |
| mean anomaly at epoch: | 284.7758° |
| orbit number at epoch: | 51379 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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