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 00082U 61004B 21021.67216227 -.00000094 00000-0 -24698-4 0 9998
2 00082 38.8559 110.3514 1174787 56.7817 314.0028 12.26048990834592
| Epoch (UTC): | 21 January 2021 16:07:54 |
| Eccentricity: | 0.1174787 |
| inclination: | 38.8559° |
| perigee height: | 633 km |
| apogee height: | 2499 km |
| right ascension of ascending node: | 110.3514° |
| argument of perigee: | 56.7817° |
| revolutions per day: | 12.26048990 |
| mean anomaly at epoch: | 314.0028° |
| orbit number at epoch: | 83459 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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