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 25400U 98043G 21295.40992867 -.00000008 00000-0 15124-4 0 9995
2 25400 98.6479 229.4251 0009702 348.5054 11.5902 14.25485195211105
| Epoch (UTC): | 22 October 2021 09:50:17 |
| Eccentricity: | 0.0009702 |
| inclination: | 98.6479° |
| perigee height: | 800 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 229.4251° |
| argument of perigee: | 348.5054° |
| revolutions per day: | 14.25485195 |
| mean anomaly at epoch: | 11.5902° |
| orbit number at epoch: | 21110 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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