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 23341.87638718 .00000038 00000-0 76809-4 0 9994
2 24278 98.5567 296.9568 0349717 326.6558 31.2983 13.53166027348674
| Epoch (UTC): | 07 December 2023 21:01:59 |
| Eccentricity: | 0.0349717 |
| inclination: | 98.5567° |
| perigee height: | 800 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 296.9568° |
| argument of perigee: | 326.6558° |
| revolutions per day: | 13.53166027 |
| mean anomaly at epoch: | 31.2983° |
| orbit number at epoch: | 34867 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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