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 00012U 59001B 24262.49698946 .00002300 00000-0 13388-2 0 9999
2 00012 32.9044 306.8664 1653531 336.6899 16.6375 11.47123545458141
| Epoch (UTC): | 18 September 2024 11:55:39 |
| Eccentricity: | 0.1653531 |
| inclination: | 32.9044° |
| perigee height: | 553 km |
| apogee height: | 3300 km |
| right ascension of ascending node: | 306.8664° |
| argument of perigee: | 336.6899° |
| revolutions per day: | 11.47123545 |
| mean anomaly at epoch: | 16.6375° |
| orbit number at epoch: | 45814 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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