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 43188U 18014J 23274.19031072 .00006658 00000-0 52062-3 0 9992
2 43188 97.6122 175.9597 0014141 164.6278 195.5378 15.01319446309454
| Epoch (UTC): | 01 October 2023 04:34:02 |
| Eccentricity: | 0.0014141 |
| inclination: | 97.6122° |
| perigee height: | 553 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 175.9597° |
| argument of perigee: | 164.6278° |
| revolutions per day: | 15.01319446 |
| mean anomaly at epoch: | 195.5378° |
| orbit number at epoch: | 30945 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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