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 23332.41026440 .00011943 00000-0 10243-2 0 9995
2 40042 98.0281 284.9071 0014272 98.5756 261.7083 14.97589872512596
| Epoch (UTC): | 28 November 2023 09:50:46 |
| Eccentricity: | 0.0014272 |
| inclination: | 98.0281° |
| perigee height: | 564 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 284.9071° |
| argument of perigee: | 98.5756° |
| revolutions per day: | 14.97589872 |
| mean anomaly at epoch: | 261.7083° |
| orbit number at epoch: | 51259 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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