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 22177.52739498 -.00000003 00000-0 36011-4 0 9993
2 24278 98.5152 199.9696 0349220 259.7410 96.4186 13.53116512276830
| Epoch (UTC): | 26 June 2022 12:39:26 |
| Eccentricity: | 0.0349220 |
| inclination: | 98.5152° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 199.9696° |
| argument of perigee: | 259.7410° |
| revolutions per day: | 13.53116512 |
| mean anomaly at epoch: | 96.4186° |
| orbit number at epoch: | 27683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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