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 22221.20998934 -.00000030 00000-0 61616-6 0 9994
2 00082 38.8611 180.0925 1172330 261.1040 85.5417 12.26021151903884
| Epoch (UTC): | 09 August 2022 05:02:23 |
| Eccentricity: | 0.1172330 |
| inclination: | 38.8611° |
| perigee height: | 635 km |
| apogee height: | 2498 km |
| right ascension of ascending node: | 180.0925° |
| argument of perigee: | 261.1040° |
| revolutions per day: | 12.26021151 |
| mean anomaly at epoch: | 85.5417° |
| orbit number at epoch: | 90388 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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