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 23332.50464234 .00001200 00000-0 62658-3 0 9991
2 00011 32.8707 4.1554 1460160 165.4830 199.2760 11.87404812424522
| Epoch (UTC): | 28 November 2023 12:06:41 |
| Eccentricity: | 0.1460160 |
| inclination: | 32.8707° |
| perigee height: | 553 km |
| apogee height: | 2923 km |
| right ascension of ascending node: | 4.1554° |
| argument of perigee: | 165.4830° |
| revolutions per day: | 11.87404812 |
| mean anomaly at epoch: | 199.2760° |
| orbit number at epoch: | 42452 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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