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 23037.38824918 .00002658 00000-0 14061-2 0 9990
2 00011 32.8793 34.9142 1463581 295.3498 50.2711 11.86464388389440
| Epoch (UTC): | 06 February 2023 09:19:04 |
| Eccentricity: | 0.1463581 |
| inclination: | 32.8793° |
| perigee height: | 553 km |
| apogee height: | 2930 km |
| right ascension of ascending node: | 34.9142° |
| argument of perigee: | 295.3498° |
| revolutions per day: | 11.86464388 |
| mean anomaly at epoch: | 50.2711° |
| orbit number at epoch: | 38944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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