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 38782U 12052A 22179.13481445 .00000395 00000-0 63735-4 0 9994
2 38782 97.6594 217.0104 0015621 283.2973 76.6499 14.76341068525456
| Epoch (UTC): | 28 June 2022 03:14:07 |
| Eccentricity: | 0.0015621 |
| inclination: | 97.6594° |
| perigee height: | 630 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 217.0104° |
| argument of perigee: | 283.2973° |
| revolutions per day: | 14.76341068 |
| mean anomaly at epoch: | 76.6499° |
| orbit number at epoch: | 52545 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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