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 40960U 15057C 22267.74518928 .00000310 00000-0 54608-4 0 9991
2 40960 97.7459 311.2304 0018368 6.3614 353.7814 14.73742240374685
| Epoch (UTC): | 24 September 2022 17:53:04 |
| Eccentricity: | 0.0018368 |
| inclination: | 97.7459° |
| perigee height: | 636 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 311.2304° |
| argument of perigee: | 6.3614° |
| revolutions per day: | 14.73742240 |
| mean anomaly at epoch: | 353.7814° |
| orbit number at epoch: | 37468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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