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 16U 58002A 24256.55997733 .00001021 00000-0 13657-2 0 9997
2 16 34.2826 3.5135 2025899 286.7877 52.1078 10.49413362621376
| Epoch (UTC): | 12 September 2024 13:26:22 |
| Eccentricity: | 0.2025899 |
| inclination: | 34.2826° |
| perigee height: | 649 km |
| apogee height: | 4220 km |
| right ascension of ascending node: | 3.5135° |
| argument of perigee: | 286.7877° |
| revolutions per day: | 10.49413362 |
| mean anomaly at epoch: | 52.1078° |
| orbit number at epoch: | 62137 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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