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 23339.42540796 .00008837 00000-0 75608-3 0 9993
2 40042 98.0302 292.1168 0014846 78.4355 281.8532 14.97767058513640
| Epoch (UTC): | 05 December 2023 10:12:35 |
| Eccentricity: | 0.0014846 |
| inclination: | 98.0302° |
| perigee height: | 563 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 292.1168° |
| argument of perigee: | 78.4355° |
| revolutions per day: | 14.97767058 |
| mean anomaly at epoch: | 281.8532° |
| orbit number at epoch: | 51364 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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