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 40021U 14033M 23090.43575896 .00015295 00000-0 13450-2 0 9996
2 40021 98.0502 52.0083 0011937 160.5764 199.5914 14.96576537477550
| Epoch (UTC): | 31 March 2023 10:27:29 |
| Eccentricity: | 0.0011937 |
| inclination: | 98.0502° |
| perigee height: | 569 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 52.0083° |
| argument of perigee: | 160.5764° |
| revolutions per day: | 14.96576537 |
| mean anomaly at epoch: | 199.5914° |
| orbit number at epoch: | 47755 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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