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 23336.81988508 .00012345 00000-0 10550-2 0 9993
2 40042 98.0299 289.4384 0014714 86.0802 274.2101 14.97715481513258
| Epoch (UTC): | 02 December 2023 19:40:38 |
| Eccentricity: | 0.0014714 |
| inclination: | 98.0299° |
| perigee height: | 564 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 289.4384° |
| argument of perigee: | 86.0802° |
| revolutions per day: | 14.97715481 |
| mean anomaly at epoch: | 274.2101° |
| orbit number at epoch: | 51325 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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