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 24276.55089925 .00000121 00000-0 16245-3 0 9997
2 24278 98.5806 197.1312 0348909 270.1933 85.9237 13.53213714389209
| Epoch (UTC): | 02 October 2024 13:13:17 |
| Eccentricity: | 0.0348909 |
| inclination: | 98.5806° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 197.1312° |
| argument of perigee: | 270.1933° |
| revolutions per day: | 13.53213714 |
| mean anomaly at epoch: | 85.9237° |
| orbit number at epoch: | 38920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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