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 39136U 13015G 23265.55862883 .00078744 00000-0 14127-2 0 9992
2 39136 64.8658 21.4570 0027221 267.5140 92.2885 15.49049343576711
| Epoch (UTC): | 22 September 2023 13:24:25 |
| Eccentricity: | 0.0027221 |
| inclination: | 64.8658° |
| perigee height: | 401 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 21.4570° |
| argument of perigee: | 267.5140° |
| revolutions per day: | 15.49049343 |
| mean anomaly at epoch: | 92.2885° |
| orbit number at epoch: | 57671 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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