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 42000U 17008BE 23083.66276812 .00043287 00000-0 12307-2 0 9995
2 42000 97.2131 141.2425 0005376 350.1030 10.0107 15.36013181338948
| Epoch (UTC): | 24 March 2023 15:54:23 |
| Eccentricity: | 0.0005376 |
| inclination: | 97.2131° |
| perigee height: | 454 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 141.2425° |
| argument of perigee: | 350.1030° |
| revolutions per day: | 15.36013181 |
| mean anomaly at epoch: | 10.0107° |
| orbit number at epoch: | 33894 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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