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 24276.91525387 .00044263 00000-0 29690-2 0 9999
2 40042 98.0822 245.9651 0014933 121.7163 238.5520 15.06599326559037
| Epoch (UTC): | 02 October 2024 21:57:57 |
| Eccentricity: | 0.0014933 |
| inclination: | 98.0822° |
| perigee height: | 536 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 245.9651° |
| argument of perigee: | 121.7163° |
| revolutions per day: | 15.06599326 |
| mean anomaly at epoch: | 238.5520° |
| orbit number at epoch: | 55903 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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