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 24278U 96046B 23331.89480552 .00000046 00000-0 84113-4 0 9992
2 24278 98.5549 288.3096 0350125 352.5487 7.0528 13.53164203347072
| Epoch (UTC): | 27 November 2023 21:28:31 |
| Eccentricity: | 0.0350125 |
| inclination: | 98.5549° |
| perigee height: | 800 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 288.3096° |
| argument of perigee: | 352.5487° |
| revolutions per day: | 13.53164203 |
| mean anomaly at epoch: | 7.0528° |
| orbit number at epoch: | 34707 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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