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 23029.39970120 .00006262 00000-0 61689-3 0 9997
2 40042 97.9938 335.5487 0014685 32.5625 327.6496 14.92336991467831
| Epoch (UTC): | 29 January 2023 09:35:34 |
| Eccentricity: | 0.0014685 |
| inclination: | 97.9938° |
| perigee height: | 580 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 335.5487° |
| argument of perigee: | 32.5625° |
| revolutions per day: | 14.92336991 |
| mean anomaly at epoch: | 327.6496° |
| orbit number at epoch: | 46783 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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