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 22590U 93020A 23266.23747410 .00000079 00000-0 66476-4 0 9998
2 22590 82.9344 161.9122 0022422 196.2281 278.0593 13.75486408529582
| Epoch (UTC): | 23 September 2023 05:41:57 |
| Eccentricity: | 0.0022422 |
| inclination: | 82.9344° |
| perigee height: | 963 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 161.9122° |
| argument of perigee: | 196.2281° |
| revolutions per day: | 13.75486408 |
| mean anomaly at epoch: | 278.0593° |
| orbit number at epoch: | 52958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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