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 04384U 70036B 22177.90729372 -.00000024 00000-0 -60424-4 0 9991
2 04384 74.0269 146.6113 0054135 280.6565 140.7848 12.39222821359945
| Epoch (UTC): | 26 June 2022 21:46:30 |
| Eccentricity: | 0.0054135 |
| inclination: | 74.0269° |
| perigee height: | 1467 km |
| apogee height: | 1552 km |
| right ascension of ascending node: | 146.6113° |
| argument of perigee: | 280.6565° |
| revolutions per day: | 12.39222821 |
| mean anomaly at epoch: | 140.7848° |
| orbit number at epoch: | 35994 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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