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 22022.57525081 -.00000038 00000-0 17332-4 0 9994
2 00082 38.8523 195.4945 1174075 22.5554 342.2678 12.26009835879503
| Epoch (UTC): | 22 January 2022 13:48:21 |
| Eccentricity: | 0.1174075 |
| inclination: | 38.8523° |
| perigee height: | 634 km |
| apogee height: | 2499 km |
| right ascension of ascending node: | 195.4945° |
| argument of perigee: | 22.5554° |
| revolutions per day: | 12.26009835 |
| mean anomaly at epoch: | 342.2678° |
| orbit number at epoch: | 87950 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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