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 23081.41303036 .00009001 00000-0 86071-3 0 9990
2 40042 98.0014 28.3914 0012024 205.1243 154.9392 14.93418438475595
| Epoch (UTC): | 22 March 2023 09:54:45 |
| Eccentricity: | 0.0012024 |
| inclination: | 98.0014° |
| perigee height: | 579 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 28.3914° |
| argument of perigee: | 205.1243° |
| revolutions per day: | 14.93418438 |
| mean anomaly at epoch: | 154.9392° |
| orbit number at epoch: | 47559 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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