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 23150.56183073 .00000896 00000-0 45413-3 0 9994
2 00011 32.8760 329.1381 1462211 215.5862 133.8011 11.87166177402898
| Epoch (UTC): | 30 May 2023 13:29:02 |
| Eccentricity: | 0.1462211 |
| inclination: | 32.8760° |
| perigee height: | 552 km |
| apogee height: | 2925 km |
| right ascension of ascending node: | 329.1381° |
| argument of perigee: | 215.5862° |
| revolutions per day: | 11.87166177 |
| mean anomaly at epoch: | 133.8011° |
| orbit number at epoch: | 40289 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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