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 40922U 15050C 22279.92386119 -.00000644 00000-0 -47208-2 0 9998
2 40922 82.4921 198.7222 0017001 98.2851 261.9760 12.42889570319266
| Epoch (UTC): | 06 October 2022 22:10:21 |
| Eccentricity: | 0.0017001 |
| inclination: | 82.4921° |
| perigee height: | 1481 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 198.7222° |
| argument of perigee: | 98.2851° |
| revolutions per day: | 12.42889570 |
| mean anomaly at epoch: | 261.9760° |
| orbit number at epoch: | 31926 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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