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 23334.41468265 .00013320 00000-0 11399-2 0 9996
2 40042 98.0293 286.9665 0014452 93.0665 267.2211 14.97644175513402
| Epoch (UTC): | 30 November 2023 09:57:08 |
| Eccentricity: | 0.0014452 |
| inclination: | 98.0293° |
| perigee height: | 564 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 286.9665° |
| argument of perigee: | 93.0665° |
| revolutions per day: | 14.97644175 |
| mean anomaly at epoch: | 267.2211° |
| orbit number at epoch: | 51340 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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