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 22183.88037154 -.00000016 00000-0 -11297-5 0 9991
2 04384 74.0276 138.8319 0054111 271.9499 147.8014 12.39222755360689
| Epoch (UTC): | 02 July 2022 21:07:44 |
| Eccentricity: | 0.0054111 |
| inclination: | 74.0276° |
| perigee height: | 1467 km |
| apogee height: | 1552 km |
| right ascension of ascending node: | 138.8319° |
| argument of perigee: | 271.9499° |
| revolutions per day: | 12.39222755 |
| mean anomaly at epoch: | 147.8014° |
| orbit number at epoch: | 36068 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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