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 39134U 13015E 22177.00297726 .00010520 00000-0 37551-3 0 9994
2 39134 64.8626 33.8295 0034939 278.3403 81.3767 15.28721368508164
| Epoch (UTC): | 26 June 2022 00:04:17 |
| Eccentricity: | 0.0034939 |
| inclination: | 64.8626° |
| perigee height: | 455 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 33.8295° |
| argument of perigee: | 278.3403° |
| revolutions per day: | 15.28721368 |
| mean anomaly at epoch: | 81.3767° |
| orbit number at epoch: | 50816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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