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 21397U 91039A 23271.84076646 .00003472 00000-0 30598-3 0 9994
2 21397 82.5173 116.0599 0018203 111.2131 249.1037 14.96056208731148
| Epoch (UTC): | 28 September 2023 20:10:42 |
| Eccentricity: | 0.0018203 |
| inclination: | 82.5173° |
| perigee height: | 566 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 116.0599° |
| argument of perigee: | 111.2131° |
| revolutions per day: | 14.96056208 |
| mean anomaly at epoch: | 249.1037° |
| orbit number at epoch: | 73114 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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