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 40382U 15004B 22335.39649755 .21214084 27327-5 21367-3 0 9990
2 40382 97.5442 156.6939 0008499 261.4045 149.6755 16.50833640440653
| Epoch (UTC): | 01 December 2022 09:30:57 |
| Eccentricity: | 0.0008499 |
| inclination: | 97.5442° |
| perigee height: | 131 km |
| apogee height: | 142 km |
| right ascension of ascending node: | 156.6939° |
| argument of perigee: | 261.4045° |
| revolutions per day: | 16.50833640 |
| mean anomaly at epoch: | 149.6755° |
| orbit number at epoch: | 44065 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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