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 40012U 14033C 22135.47941781 .00001618 00000-0 24303-3 0 9993
2 40012 97.6627 325.2067 0056096 265.7466 93.7332 14.74805304425120
| Epoch (UTC): | 15 May 2022 11:30:21 |
| Eccentricity: | 0.0056096 |
| inclination: | 97.6627° |
| perigee height: | 606 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 325.2067° |
| argument of perigee: | 265.7466° |
| revolutions per day: | 14.74805304 |
| mean anomaly at epoch: | 93.7332° |
| orbit number at epoch: | 42512 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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