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 43678U 18084H 23332.57308080 .00003579 00000-0 33959-3 0 9999
2 43678 98.0453 120.1855 0008933 347.0788 13.0200 14.94179373276808
| Epoch (UTC): | 28 November 2023 13:45:14 |
| Eccentricity: | 0.0008933 |
| inclination: | 98.0453° |
| perigee height: | 579 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 120.1855° |
| argument of perigee: | 347.0788° |
| revolutions per day: | 14.94179373 |
| mean anomaly at epoch: | 13.0200° |
| orbit number at epoch: | 27680 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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