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 00011U 59001A 23331.49578116 .00001016 00000-0 53002-3 0 9991
2 00011 32.8703 7.9547 1460184 159.7706 206.7414 11.87401374424402
| Epoch (UTC): | 27 November 2023 11:53:55 |
| Eccentricity: | 0.1460184 |
| inclination: | 32.8703° |
| perigee height: | 552 km |
| apogee height: | 2923 km |
| right ascension of ascending node: | 7.9547° |
| argument of perigee: | 159.7706° |
| revolutions per day: | 11.87401374 |
| mean anomaly at epoch: | 206.7414° |
| orbit number at epoch: | 42440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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