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 11574U 79089B 23156.41118094 .00000270 00000-0 91647-4 0 9996
2 11574 74.0674 155.6434 0016832 228.3979 131.5735 14.41157355290794
| Epoch (UTC): | 05 June 2023 09:52:06 |
| Eccentricity: | 0.0016832 |
| inclination: | 74.0674° |
| perigee height: | 742 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 155.6434° |
| argument of perigee: | 228.3979° |
| revolutions per day: | 14.41157355 |
| mean anomaly at epoch: | 131.5735° |
| orbit number at epoch: | 29079 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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