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 23405U 94077B 22144.37226672 -.00000155 00000-0 -54917-4 0 9992
2 23405 70.9842 26.1363 0000872 165.4313 194.6835 14.15255404420482
| Epoch (UTC): | 24 May 2022 08:56:03 |
| Eccentricity: | 0.0000872 |
| inclination: | 70.9842° |
| perigee height: | 841 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 26.1363° |
| argument of perigee: | 165.4313° |
| revolutions per day: | 14.15255404 |
| mean anomaly at epoch: | 194.6835° |
| orbit number at epoch: | 42048 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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