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 40907U 15049J 22175.80337097 .00006053 00000-0 28518-3 0 9994
2 40907 97.4906 179.1438 0012249 337.5569 148.1237 15.19818993374088
| Epoch (UTC): | 24 June 2022 19:16:51 |
| Eccentricity: | 0.0012249 |
| inclination: | 97.4906° |
| perigee height: | 498 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 179.1438° |
| argument of perigee: | 337.5569° |
| revolutions per day: | 15.19818993 |
| mean anomaly at epoch: | 148.1237° |
| orbit number at epoch: | 37408 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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