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 21101.92460431 -.00000122 00000-0 -47750-4 0 9999
2 00082 38.8543 173.1840 1175492 84.1031 289.2119 12.26040766844443
| Epoch (UTC): | 11 April 2021 22:11:25 |
| Eccentricity: | 0.1175492 |
| inclination: | 38.8543° |
| perigee height: | 632 km |
| apogee height: | 2500 km |
| right ascension of ascending node: | 173.1840° |
| argument of perigee: | 84.1031° |
| revolutions per day: | 12.26040766 |
| mean anomaly at epoch: | 289.2119° |
| orbit number at epoch: | 84444 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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