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 40617U 15023A 22222.97416773 .00000089 00000-0 00000+0 0 9999
2 40617 0.0194 116.4543 0002665 21.9319 223.7577 1.00274033 26733
| Epoch (UTC): | 10 August 2022 23:22:48 |
| Eccentricity: | 0.0002665 |
| inclination: | 0.0194° |
| perigee height: | 35774 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 116.4543° |
| argument of perigee: | 21.9319° |
| revolutions per day: | 1.00274033 |
| mean anomaly at epoch: | 223.7577° |
| orbit number at epoch: | 2673 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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