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 23160.73923006 .00000734 00000-0 36805-3 0 9998
2 00011 32.8792 290.8382 1462368 273.1566 70.3281 11.87183570404108
| Epoch (UTC): | 09 June 2023 17:44:29 |
| Eccentricity: | 0.1462368 |
| inclination: | 32.8792° |
| perigee height: | 552 km |
| apogee height: | 2926 km |
| right ascension of ascending node: | 290.8382° |
| argument of perigee: | 273.1566° |
| revolutions per day: | 11.87183570 |
| mean anomaly at epoch: | 70.3281° |
| orbit number at epoch: | 40410 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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