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 22176.52616942 .00005866 00000-0 27641-3 0 9990
2 40907 97.4904 179.8611 0012234 334.7576 143.0862 15.19826278374192
| Epoch (UTC): | 25 June 2022 12:37:41 |
| Eccentricity: | 0.0012234 |
| inclination: | 97.4904° |
| perigee height: | 498 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 179.8611° |
| argument of perigee: | 334.7576° |
| revolutions per day: | 15.19826278 |
| mean anomaly at epoch: | 143.0862° |
| orbit number at epoch: | 37419 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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