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 23081.23414710 -.00000005 00000-0 34044-4 0 9999
2 24278 98.5226 71.6634 0349183 282.5145 73.7149 13.53138982313426
| Epoch (UTC): | 22 March 2023 05:37:10 |
| Eccentricity: | 0.0349183 |
| inclination: | 98.5226° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 71.6634° |
| argument of perigee: | 282.5145° |
| revolutions per day: | 13.53138982 |
| mean anomaly at epoch: | 73.7149° |
| orbit number at epoch: | 31342 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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